BLbluestaq
Maneuver

GET /udl/maneuver

Changed on

Service operation to dynamically query data by a variety of query parameters not specified in this API documentation. See the queryhelp operation (/udl/<datatype>/queryhelp) for more details on valid/required query parameter information.

Request

  • Base URL
    https://unifieddatalibrary.com
  • URL
    https://unifieddatalibrary.com/udl/maneuver
  • Auth
    none declared

Query parameters

eventStartTimestring date-time required

Maneuver event start time in ISO 8601 UTC with microsecond precision. For maneuvers without start and end times, the start time is considered to be the maneuver event time. (YYYY-MM-DDTHH:MM:SS.ssssssZ)

firstResultinteger
maxResultsinteger

Response

OK

idstring

Unique identifier of the record, auto-generated by the system.

classificationMarkingstring required

Classification marking of the data in IC/CAPCO Portion-marked format.

satNointeger

Satellite/Catalog number of the target on-orbit object.

reportTimestring date-time

The time that the report or alert of this maneuver was generated, in ISO 8601 UTC format.

eventStartTimestring date-time required

Maneuver event start time in ISO 8601 UTC with microsecond precision. For maneuvers without start and end times, the start time is considered to be the maneuver event time.

eventEndTimestring date-time

Maneuver event end time in ISO 8601 UTC with microsecond precision.

totalBurnTimenumber double

The estimated total active burn time of a maneuver, in seconds. This includes the sum of all burns in numAccelPoints. Not to be confused with the total duration of the maneuver.

odFitEndTimestring date-time

Maneuver orbit determination fit data end time in ISO 8601 UTC with microsecond precision.

idOnOrbitstring

Target maneuvering on-orbit object. For the public catalog, the idOnOrbit is typically the satellite number as a string, but may be a UUID for analyst or other unknown or untracked satellites.

idSensorstring

Optional ID of the sensor that detected this maneuver (for example, if detected by passive RF anomalies).

uctboolean

Boolean indicating this maneuver was unable to be correlated to a known object. This flag should only be set to true by data providers after an attempt to correlate to an on-orbit object was made and failed. If unable to correlate, the 'origObjectId' field may be populated with an internal data provider specific identifier.

maneuverUncnumber double

Uncertainty in the occurrence of this maneuver (0 - 1).

characterizationstring

Optional purpose of the maneuver if known (e.g. North-South Station Keeping, East-West Station Keeping, Longitude Shift, Unknown).

characterizationUncnumber double

Uncertainty in the characterization or purpose assessment of this maneuver (0 - 1).

eventIdstring

Optional source-provided identifier for this maneuver event. In the case where multiple maneuver records are submitted for the same event, this field can be used to tie them together to the same event.

origObjectIdstring

Identifier provided by source to indicate the target on-orbit object performing this maneuver. This may be an internal identifier and not necessarily a valid satellite number/ID.

origSensorIdstring

Optional identifier provided by source to indicate the sensor identifier used to detect this event. This may be an internal identifier and not necessarily a valid sensor ID.

statusstring

Status of this maneuver (CANCELLED, PLANNED, POSSIBLE, REDACTED, VERIFIED).

CANCELLED: A previously planned maneuver whose execution was cancelled.

PLANNED: A maneuver planned to take place at the eventStartTime.

POSSIBLE: A possible maneuver detected by observation of the spacecraft or by evaluation of the spacecraft orbit.

REDACTED: A redaction of a reported possible maneuver that has been determined to have not taken place after further observation/evaluation.

VERIFIED: A maneuver whose execution has been verified, either by the owner/operator or observation/evaluation.

deltaPosnumber double

Magnitude, in km, of the difference in the pre- and post-maneuver position vectors at the maneuver event time.

deltaPosUnumber double

Magnitude, in km, of the difference in the pre- and post-maneuver position vectors in the direction of the pre-maneuver 'U' unit vector at the maneuver event time.

deltaPosVnumber double

Magnitude, in km, of the difference in the pre- and post-maneuver position vectors in the direction of the pre-maneuver 'V' unit vector at the maneuver event time.

deltaPosWnumber double

Magnitude, in km, of the difference in the pre- and post-maneuver position vectors in the direction of the pre-maneuver 'W' unit vector at the maneuver event time.

deltaVelnumber double

Magnitude, in km/sec, of the difference in the pre- and post-maneuver velocity vectors at the maneuver event time.

deltaVelUnumber double

Magnitude, in km/sec, of the difference in the pre- and post-maneuver velocity vectors in the direction of the pre-maneuver 'U' unit vector at the maneuver event time.

deltaVelVnumber double

Magnitude, in km/sec, of the difference in the pre- and post-maneuver velocity vectors in the direction of the pre-maneuver 'V' unit vector at the maneuver event time.

deltaVelWnumber double

Magnitude, in km/sec, of the difference in the pre- and post-maneuver velocity vectors in the direction of the pre-maneuver 'W' unit vector at the maneuver event time.

deltaMassnumber double

Difference in mass before and after the maneuver, in kg.

preEventIdElsetstring

Optional identifier of the element set for the pre-maneuver orbit.

preEventIdStateVectorstring

Optional identifier of the state vector for the pre-maneuver trajectory of the spacecraft.

prePosXnumber double

Pre-event X component of position in ECI space, in km.

prePosYnumber double

Pre-event Y component of position in ECI space, in km.

prePosZnumber double

Pre-event Z component of position in ECI space, in km.

preVelXnumber double

Pre-event X component of velocity in ECI space, in km/sec.

preVelYnumber double

Pre-event Y component of velocity in ECI space, in km/sec.

preVelZnumber double

Pre-event Z component of velocity in ECI space, in km/sec.

preRadiationPressCoeffnumber double

Pre-event radiation pressure coefficient. The units of the radiation pressure coefficient vary depending on provider. Users should consult the data provider to verify the units of the radiation pressure coefficient.

preBallisticCoeffnumber double

Pre-event ballistic coefficient. The units of the ballistic coefficient vary depending on provider. Users should consult the data provider to verify the units of the ballistic coefficient.

preApogeenumber double

Pre-event spacecraft apogee (measured from Earth center), in kilometers.

prePerigeenumber double

Pre-event spacecraft perigee (measured from Earth center), in kilometers.

preInclinationnumber double

Pre-event spacecraft orbital inclination, in degrees. 0-180.

preEccentricitynumber double

Pre-event spacecraft eccentricity.

prePeriodnumber double

Pre-event spacecraft orbital period, in minutes.

preRAANnumber double

Pre-event spacecraft Right Ascension of the Ascending Node (RAAN), in degrees.

preSMAnumber double

Pre-event spacecraft orbital Semi-Major Axis (SMA), in kilometers.

preGeoLongitudenumber double

Pre-event spacecraft WGS-84 GEO belt longitude, represented as -180 to 180 degrees (negative values west of Prime Meridian).

preDriftRatenumber double

Pre-event GEO drift rate of the spacecraft, in degrees per day. Negative values indicate westward drift.

preSigmaUnumber double

Pre-event standard deviation, in kilometers, of spacecraft position in the 'U' unit vector direction.

preSigmaVnumber double

Pre-event standard deviation, in kilometers, of spacecraft position in the 'V' unit vector direction.

preSigmaWnumber double

Pre-event standard deviation, in kilometers, of spacecraft position in the 'W' unit vector direction.

postEventIdElsetstring

Optional identifier of the element set for the post-maneuver orbit.

postEventIdStateVectorstring

Optional identifier of the state vector for the post-maneuver trajectory of the spacecraft.

postPosXnumber double

Post-event X component of position in ECI space, in km.

postPosYnumber double

Post-event Y component of position in ECI space, in km.

postPosZnumber double

Post-event Z component of position in ECI space, in km.

postVelXnumber double

Post-event X component of velocity in ECI space, in km/sec.

postVelYnumber double

Post-event Y component of velocity in ECI space, in km/sec.

postVelZnumber double

Post-event Z component of velocity in ECI space, in km/sec.

postRadiationPressCoeffnumber double

Post-event radiation pressure coefficient. The units of the radiation pressure coefficient vary depending on provider. Users should consult the data provider to verify the units of the radiation pressure coefficient.

postBallisticCoeffnumber double

Post-event ballistic coefficient. The units of the ballistic coefficient vary depending on provider. Users should consult the data provider to verify the units of the ballistic coefficient.

postApogeenumber double

Post-event spacecraft apogee (measured from Earth center), in kilometers.

postPerigeenumber double

Post-event spacecraft perigee (measured from Earth center), in kilometers.

postInclinationnumber double

Post-event spacecraft orbital inclination, in degrees. 0-180.

postEccentricitynumber double

Post-event spacecraft eccentricity.

postPeriodnumber double

Post-event spacecraft orbital period, in minutes.

postRAANnumber double

Post-event spacecraft Right Ascension of the Ascending Node (RAAN), in degrees.

postSMAnumber double

Post-event spacecraft Semi-Major Axis (SMA), in kilometers.

postGeoLongitudenumber double

Post-event spacecraft WGS-84 GEO belt longitude, represented as -180 to 180 degrees (negative values west of Prime Meridian).

postDriftRatenumber double

Post-event GEO drift rate of the spacecraft, in degrees per day. Negative values indicate westward drift.

postSigmaUnumber double

Post-event standard deviation, in kilometers, of spacecraft position in the 'U' unit vector direction.

postSigmaVnumber double

Post-event standard deviation, in kilometers, of spacecraft position in the 'V' unit vector direction.

postSigmaWnumber double

Post-event standard deviation, in kilometers, of spacecraft position in the 'W' unit vector direction.

covnumber[]

Optional maneuver cross-track/radial/in-track covariance array, in meter and second based units, in the following order: CR_R, CI_R, CI_I, CC_R, CC_I, CC_C, CT_R, CT_I, CT_C, CT_T.

postMassnumber double

Estimated mass of the object following the maneuver, in kg.

postAreanumber double

Estimated area of the object following the maneuver, in meters squared.

numObsinteger

Number of observations used to generate the maneuver data.

descriptionstring

Description and notes of the maneuver.

descriptorstring

Optional source-provided and searchable metadata or descriptor of the data.

stateModelstring

Name of the state model used to generate the maneuver data.

stateModelVersionnumber double

Version of the state model used to generate the maneuver data.

numAccelPointsinteger

The total number of estimated acceleration points during the maneuver.

mnvrAccelTimesnumber[]

Array of elapsed times, in seconds from maneuver start time, at which each acceleration point is estimated. Number of elements must match the numAccelPoints.

mnvrAccelsnumber[]

Array of estimated acceleration values, in meters per second squared. Number of elements must match the numAccelPoints.

mnvrAccelUncsnumber[]

Array of the 1-sigma uncertainties in estimated accelerations, in meters per second squared. Number of elements must match the numAccelPoints.

sourcestring required

Source of the data.

originstring

Originating system or organization which produced the data, if different from the source. The origin may be different than the source if the source was a mediating system which forwarded the data on behalf of the origin system. If null, the source may be assumed to be the origin.

dataMode'REAL' | 'TEST' | 'SIMULATED' | 'EXERCISE' required

Indicator of whether the data is REAL, TEST, EXERCISE, or SIMULATED data:

REAL: Data collected or produced that pertains to real-world objects, events, and analysis.

TEST: Specific datasets used to evaluate compliance with specifications and requirements, and for validating technical, functional, and performance characteristics.

EXERCISE: Data pertaining to a government or military exercise. The data may include both real and simulated data.

SIMULATED: Synthetic data generated by a model to mimic real-world datasets.

createdAtstring date-time

Time the row was created in the database, auto-populated by the system.

createdBystring

Application user who created the row in the database, auto-populated by the system.

algorithmstring

Optional algorithm used to produce this record.

transactionIdstring

Optional identifier to track a commercial or marketplace transaction executed to produce this data.

origNetworkstring

The originating source network on which this record was created, auto-populated by the system.

Example response

[
  {
    "id": "MANEUVER-ID",
    "classificationMarking": "U",
    "satNo": 12,
    "reportTime": "2023-11-16T04:15:00.000100Z",
    "eventStartTime": "2023-11-16T01:05:16.835689Z",
    "eventEndTime": "2023-11-16T01:09:01.350012Z",
    "totalBurnTime": 600.72,
    "odFitEndTime": "2023-11-16T03:55:51.000000Z",
    "idOnOrbit": "12",
    "idSensor": "SENSOR-ID",
    "maneuverUnc": 0.5,
    "characterization": "North-South Station Keeping",
    "characterizationUnc": 0.15,
    "eventId": "EVENT-ID",
    "origObjectId": "ORIGOBJECT-ID",
    "origSensorId": "ORIGSENSOR-ID",
    "status": "POSSIBLE",
    "deltaPos": 0.715998327,
    "deltaPosU": -0.022172844,
    "deltaPosV": -0.033700154,
    "deltaPosW": -0.714861014,
    "deltaVel": 0.000631505,
    "deltaVelU": 0.0000350165629389647,
    "deltaVelV": 0.000544413,
    "deltaVelW": -0.000318099,
    "deltaMass": 0.15,
    "preEventIdElset": "80e544b7-6a17-4554-8abf-7301e98f8e5d",
    "preEventElset": {
      "idElset": "ELSET-ID",
      "classificationMarking": "U",
      "satNo": 12,
      "epoch": "2018-01-01T16:00:00.123456Z",
      "meanMotion": 1.1,
      "idOnOrbit": "ONORBIT-ID",
      "eccentricity": 0.333,
      "inclination": 45.1,
      "raan": 1.1,
      "argOfPerigee": 1.1,
      "meanAnomaly": 179.1,
      "revNo": 111,
      "bStar": 1.1,
      "agom": 0.0126,
      "ballisticCoeff": 0.00815,
      "meanMotionDot": 1.1,
      "meanMotionDDot": 1.1,
      "semiMajorAxis": 1.1,
      "period": 1.1,
      "apogee": 1.1,
      "perigee": 1.1,
      "origObjectId": "ORIGOBJECT-ID",
      "idOrbitDetermination": "026dd511-8ba5-47d3-9909-836149f87686",
      "line1": "Example line1",
      "line2": "Example line2",
      "descriptor": "Example description",
      "createdAt": "2018-01-01T16:00:00.123Z",
      "createdBy": "some.user",
      "origin": "THIRD_PARTY_DATASOURCE",
      "sourceDL": "AXE",
      "source": "Bluestaq",
      "dataMode": "TEST",
      "algorithm": "Example algorithm",
      "transactionId": "TRANSACTION-ID",
      "ephemType": 1,
      "origNetwork": "OPS1"
    },
    "preEventIdStateVector": "6e291992-8ae3-4592-bb0f-055715bf4803",
    "preEventStateVector": {
      "idStateVector": "STATEVECTOR-ID",
      "classificationMarking": "U",
      "epoch": "2018-01-01T16:00:00.123456Z",
      "pedigree": "CONJUNCTION",
      "idOnOrbit": "ONORBIT-ID",
      "satNo": 12,
      "origObjectId": "ORIGOBJECT-ID",
      "idOrbitDetermination": "026dd511-8ba5-47d3-9909-836149f87686",
      "msgTs": "2018-01-01T16:00:00.123456Z",
      "uct": true,
      "xpos": -1118.577381,
      "ypos": 3026.231084,
      "zpos": 6167.831808,
      "xvel": -4.25242784,
      "yvel": 5.291107434,
      "zvel": -3.356493869,
      "xaccel": -2.12621392,
      "yaccel": 2.645553717,
      "zaccel": -1.06310696,
      "referenceFrame": "J2000",
      "cov": [
        1.1,
        2.4,
        3.8,
        4.2,
        5.5,
        6
      ],
      "covReferenceFrame": "J2000",
      "covMethod": "CALCULATED",
      "eqCov": [
        1.1,
        2.2
      ],
      "xposAlt1": -1145.688502,
      "yposAlt1": 3020.729572,
      "zposAlt1": 6165.55187,
      "xvelAlt1": -4.270832252,
      "yvelAlt1": 5.27074276,
      "zvelAlt1": -3.365155181,
      "alt1ReferenceFrame": "TEME",
      "xposAlt2": -1456.915926,
      "yposAlt2": -2883.540406,
      "zposAlt2": 6165.55187,
      "xvelAlt2": -1.219814294,
      "yvelAlt2": -6.602080212,
      "zvelAlt2": -3.365155181,
      "alt2ReferenceFrame": "EFG/TDR",
      "posUnc": 0.333399744452,
      "velUnc": 0.000004,
      "mass": 164.5,
      "area": 5.065,
      "solarRadPressCoeff": 0.0244394,
      "dragCoeff": 0.0224391269775,
      "dragArea": 4.739,
      "revNo": 7205,
      "geopotentialModel": "EGM-96",
      "dragModel": "JAC70",
      "lunarSolar": true,
      "solarRadPress": true,
      "srpArea": 4.311,
      "solidEarthTides": true,
      "inTrackThrust": true,
      "bDot": 1.23,
      "edr": 1.23,
      "thrustAccel": 1.23,
      "cmOffset": 1.23,
      "lastObStart": "2022-11-09T11:20:21.247192Z",
      "lastObEnd": "2022-11-09T11:20:21.247192Z",
      "obsAvailable": 376,
      "obsUsed": 374,
      "tracksAvail": 163,
      "tracksUsed": 163,
      "recODSpan": 3.5,
      "actualODSpan": 3.5,
      "residualsAcc": 99.5,
      "solarFluxF10": 1.23,
      "solarFluxF10Avg": 1.23,
      "solarFluxAPAvg": 1.23,
      "taiUtc": 1.23,
      "ut1Utc": 1.23,
      "ut1Rate": 1.23,
      "polarMotionX": 1.23,
      "polarMotionY": 1.23,
      "iau1980Terms": 4,
      "leapSecondTime": "2021-01-01T01:01:01.123Z",
      "integratorMode": "integratorMode",
      "partials": "ANALYTIC",
      "stepMode": "AUTO",
      "fixedStep": true,
      "stepSizeSelection": "AUTO",
      "stepSize": 1.23,
      "errorControl": 1.23,
      "sigmaPosUVW": [
        1.23,
        4.56
      ],
      "sigmaVelUVW": [
        1.23,
        4.56
      ],
      "rms": 0.991,
      "source": "Bluestaq",
      "origin": "THIRD_PARTY_DATASOURCE",
      "dataMode": "TEST",
      "algorithm": "SAMPLE_ALGORITHM",
      "createdAt": "2018-01-01T16:00:00.123Z",
      "createdBy": "some.user",
      "descriptor": "descriptor",
      "missionCenter": "Mission Center A",
      "transactionId": "transactionId",
      "origNetwork": "OPS1",
      "sourceDL": "AXE"
    },
    "prePosX": 3584.432545,
    "prePosY": 42028.43245,
    "prePosZ": -1.97765,
    "preVelX": -2.543266,
    "preVelY": 0.24876,
    "preVelZ": 0.0067352,
    "preRadiationPressCoeff": 4.51e-7,
    "preBallisticCoeff": 0.000437116,
    "preApogee": 35802,
    "prePerigee": 35786.5,
    "preInclination": 0.0336,
    "preEccentricity": 0.00017,
    "prePeriod": 1436.12,
    "preRAAN": 98.3336,
    "preSMA": 42165.1,
    "preGeoLongitude": -93.12,
    "preDriftRate": -0.0125,
    "preSigmaU": 0.215,
    "preSigmaV": 1.97,
    "preSigmaW": 0.208,
    "postEventIdElset": "225adf4c-8606-40a8-929e-63e22cffe220",
    "postEventElset": {
      "idElset": "ELSET-ID",
      "classificationMarking": "U",
      "satNo": 12,
      "epoch": "2018-01-01T16:00:00.123456Z",
      "meanMotion": 1.1,
      "idOnOrbit": "ONORBIT-ID",
      "eccentricity": 0.333,
      "inclination": 45.1,
      "raan": 1.1,
      "argOfPerigee": 1.1,
      "meanAnomaly": 179.1,
      "revNo": 111,
      "bStar": 1.1,
      "agom": 0.0126,
      "ballisticCoeff": 0.00815,
      "meanMotionDot": 1.1,
      "meanMotionDDot": 1.1,
      "semiMajorAxis": 1.1,
      "period": 1.1,
      "apogee": 1.1,
      "perigee": 1.1,
      "origObjectId": "ORIGOBJECT-ID",
      "idOrbitDetermination": "026dd511-8ba5-47d3-9909-836149f87686",
      "line1": "Example line1",
      "line2": "Example line2",
      "descriptor": "Example description",
      "createdAt": "2018-01-01T16:00:00.123Z",
      "createdBy": "some.user",
      "origin": "THIRD_PARTY_DATASOURCE",
      "sourceDL": "AXE",
      "source": "Bluestaq",
      "dataMode": "TEST",
      "algorithm": "Example algorithm",
      "transactionId": "TRANSACTION-ID",
      "ephemType": 1,
      "origNetwork": "OPS1"
    },
    "postEventIdStateVector": "d83a23f8-1496-485a-bd88-ec5808c73299",
    "postEventStateVector": {
      "idStateVector": "STATEVECTOR-ID",
      "classificationMarking": "U",
      "epoch": "2018-01-01T16:00:00.123456Z",
      "pedigree": "CONJUNCTION",
      "idOnOrbit": "ONORBIT-ID",
      "satNo": 12,
      "origObjectId": "ORIGOBJECT-ID",
      "idOrbitDetermination": "026dd511-8ba5-47d3-9909-836149f87686",
      "msgTs": "2018-01-01T16:00:00.123456Z",
      "uct": true,
      "xpos": -1118.577381,
      "ypos": 3026.231084,
      "zpos": 6167.831808,
      "xvel": -4.25242784,
      "yvel": 5.291107434,
      "zvel": -3.356493869,
      "xaccel": -2.12621392,
      "yaccel": 2.645553717,
      "zaccel": -1.06310696,
      "referenceFrame": "J2000",
      "cov": [
        1.1,
        2.4,
        3.8,
        4.2,
        5.5,
        6
      ],
      "covReferenceFrame": "J2000",
      "covMethod": "CALCULATED",
      "eqCov": [
        1.1,
        2.2
      ],
      "xposAlt1": -1145.688502,
      "yposAlt1": 3020.729572,
      "zposAlt1": 6165.55187,
      "xvelAlt1": -4.270832252,
      "yvelAlt1": 5.27074276,
      "zvelAlt1": -3.365155181,
      "alt1ReferenceFrame": "TEME",
      "xposAlt2": -1456.915926,
      "yposAlt2": -2883.540406,
      "zposAlt2": 6165.55187,
      "xvelAlt2": -1.219814294,
      "yvelAlt2": -6.602080212,
      "zvelAlt2": -3.365155181,
      "alt2ReferenceFrame": "EFG/TDR",
      "posUnc": 0.333399744452,
      "velUnc": 0.000004,
      "mass": 164.5,
      "area": 5.065,
      "solarRadPressCoeff": 0.0244394,
      "dragCoeff": 0.0224391269775,
      "dragArea": 4.739,
      "revNo": 7205,
      "geopotentialModel": "EGM-96",
      "dragModel": "JAC70",
      "lunarSolar": true,
      "solarRadPress": true,
      "srpArea": 4.311,
      "solidEarthTides": true,
      "inTrackThrust": true,
      "bDot": 1.23,
      "edr": 1.23,
      "thrustAccel": 1.23,
      "cmOffset": 1.23,
      "lastObStart": "2022-11-09T11:20:21.247192Z",
      "lastObEnd": "2022-11-09T11:20:21.247192Z",
      "obsAvailable": 376,
      "obsUsed": 374,
      "tracksAvail": 163,
      "tracksUsed": 163,
      "recODSpan": 3.5,
      "actualODSpan": 3.5,
      "residualsAcc": 99.5,
      "solarFluxF10": 1.23,
      "solarFluxF10Avg": 1.23,
      "solarFluxAPAvg": 1.23,
      "taiUtc": 1.23,
      "ut1Utc": 1.23,
      "ut1Rate": 1.23,
      "polarMotionX": 1.23,
      "polarMotionY": 1.23,
      "iau1980Terms": 4,
      "leapSecondTime": "2021-01-01T01:01:01.123Z",
      "integratorMode": "integratorMode",
      "partials": "ANALYTIC",
      "stepMode": "AUTO",
      "fixedStep": true,
      "stepSizeSelection": "AUTO",
      "stepSize": 1.23,
      "errorControl": 1.23,
      "sigmaPosUVW": [
        1.23,
        4.56
      ],
      "sigmaVelUVW": [
        1.23,
        4.56
      ],
      "rms": 0.991,
      "source": "Bluestaq",
      "origin": "THIRD_PARTY_DATASOURCE",
      "dataMode": "TEST",
      "algorithm": "SAMPLE_ALGORITHM",
      "createdAt": "2018-01-01T16:00:00.123Z",
      "createdBy": "some.user",
      "descriptor": "descriptor",
      "missionCenter": "Mission Center A",
      "transactionId": "transactionId",
      "origNetwork": "OPS1",
      "sourceDL": "AXE"
    },
    "postPosX": 3589.351957,
    "postPosY": 42017.26823,
    "postPosZ": -1.27161796,
    "postVelX": -3.063152826,
    "postVelY": 0.261586769,
    "postVelZ": 0.006842148,
    "postRadiationPressCoeff": 4.51e-7,
    "postBallisticCoeff": 0.000433209,
    "postApogee": 35800.1,
    "postPerigee": 35787.9,
    "postInclination": 0.0327,
    "postEccentricity": 0.000164,
    "postPeriod": 1436.01,
    "postRAAN": 98.3335,
    "postSMA": 42164.87,
    "postGeoLongitude": -93.15,
    "postDriftRate": -0.0125,
    "postSigmaU": 12.285,
    "postSigmaV": 71.339,
    "postSigmaW": 12.77,
    "cov": [
      1.1,
      2.4,
      3.4,
      4.1,
      5.6,
      6.2,
      7.9,
      8,
      9.2,
      10.1
    ],
    "postMass": 1844.5,
    "postArea": 35.77,
    "numObs": 10,
    "description": "Example notes",
    "descriptor": "Example descriptor",
    "stateModel": "Example name",
    "stateModelVersion": 3,
    "numAccelPoints": 3,
    "mnvrAccelTimes": [
      10.25,
      50.56,
      150.78
    ],
    "mnvrAccels": [
      0.05,
      0.1,
      0.05
    ],
    "mnvrAccelUncs": [
      0.0005,
      0.001,
      0.0005
    ],
    "source": "Bluestaq",
    "origin": "THIRD_PARTY_DATASOURCE",
    "dataMode": "TEST",
    "createdAt": "2018-01-01T16:00:00.123Z",
    "createdBy": "some.user",
    "algorithm": "Example algorithm",
    "transactionId": "TRANSACTION-ID",
    "origNetwork": "OPS1"
  }
]

Changes

  • bd17bc53681eRevision changes
    • info

      added the optional property // to the response with the status

    • info

      added the optional property // to the response with the status

  • 09bd422d5ac1Revision changes
    • warning

      added the new ECR/ECEF enum value to the // response property for the response status

    • warning

      added the new ECR/ECEF enum value to the // response property for the response status

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