GET /udl/conjunction/{id}

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

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

Unique identifier of the primary satellite on-orbit object, if correlated.

Unique identifier of the secondary satellite on-orbit object, if correlated.

The type of data represented in this conjunction record (e.g. CONJUNCTION, CARA-WORKLIST, etc.). If type is null the record is assumed to be a Conjunction.

Time of closest approach (TCA) in UTC.

Distance between objects at Time of Closest Approach (TCA) in meters.

Probability of Collision is the probability (denoted p, where 0.0<=p<=1.0), that Object1 and Object2 will collide.

The method that was used to calculate the collision probability, ex. FOSTER-1992.

The filename of the primary (object1) ephemeris used in the screening, if applicable.

Unique identifier of the parent Ephemeris Set of the primary (object1) ephemeris used in the screening, if applicable.

The filename of the secondary (object2) ephemeris used in the screening, if applicable.

Unique identifier of the parent Ephemeris Set of the secondary (object2) ephemeris used in the screening, if applicable.

Distance between objects along Radial Vector at Time of Closest Approach in meters.

Distance between objects along Tangential Vector in meters.

Distance between objects along Normal vector in meters.

Closing velocity magnitude (relative speed) at Time of Closest Approach in meters/sec.

Closing velocity between objects along Radial Vector at Time of Closest Approach in meters/sec.

Closing velocity between objects along Tangential Vector in meters/sec.

Closing velocity between objects along Normal Vector in meters/sec.

The start time in UTC of the screening period for the conjunction assessment.

The stop time in UTC of the screening period for the conjunction assessment.

Component size of screen in X component of RTN (Radial, Transverse and Normal) frame in meters.

Component size of screen in Y component of RTN (Radial, Transverse and Normal) frame in meters.

Component size of screen in Z component of RTN (Radial, Transverse and Normal) frame in meters.

The shape (BOX, ELLIPSOID) of the screening volume.

The time at which the secondary (object2) enters the screening volume, in ISO 8601 UTC format with microsecond precision.

The time at which the secondary (object2) exits the screening volume, in ISO 8601 UTC format with microsecond precision.

Penetration Level Sigma.

Optional ID of the UDL State Vector at TCA of the primary object. When performing a create, this id will be ignored in favor of the UDL generated id of the stateVector1.

Time of last positive metric observation of the primary satellite.

The value of the primary (object1) Area times the drag coefficient over the object Mass, expressed in m^2/kg, used for propagation of the primary state vector and covariance to TCA.

The value of the primary (object1) Area times the solar radiation pressure coefficient over the object Mass, expressed in m^2/kg, used for propagation of the primary state vector and covariance to TCA. This parameter is sometimes referred to as AGOM.

The primary (object1) acceleration, expressed in m/s^2, due to in-track thrust used to propagate the primary state vector and covariance to TCA.

Optional ID of the UDL State Vector at TCA of the secondary object. When performing a create, this id will be ignored in favor of the UDL generated id of the stateVector2.

Time of last positive metric observation of the secondary satellite.

The value of the secondary (object2) Area times the drag coefficient over the object Mass, expressed in m^2/kg, used for propagation of the primary state vector and covariance to TCA.

The value of the secondary (object2) Area times the solar radiation pressure coefficient over the object Mass, expressed in m^2/kg, used for propagation of the primary state vector and covariance to TCA. This parameter is sometimes referred to as AGOM.

The secondary (object2) acceleration, expressed in m/s^2, due to in-track thrust used to propagate the primary state vector and covariance to TCA.

Additional notes from data providers.

Commander's critical information requirements notes.

Emergency comments.

Flag indicating if State department was notified.

Flag indicating if owner was contacted.

Link to filename associated with JMS record.

Spacecraft name(s) for which the Collision message is provided.

User-provided message ID.

Used for probability of collision calculation, not Warning/Alert Threshold notifications.

Used for probability of collision calculation, not Warning/Alert Threshold notifications.

Used for probability of collision calculation, not Warning/Alert Threshold notifications.

Used for probability of collision calculation, not Warning/Alert Threshold notifications.

Used for probability of collision calculation, not Warning/Alert Threshold notifications.

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

Source of the data.

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.

Creating agency or owner/operator (may be different than provider who submitted the conjunction message).

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

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

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.

Time the row was created in the database.

Application user who created the row in the database.

Satellite/catalog number of the target on-orbit primary object.

Satellite/catalog number of the target on-orbit secondary object.

Optional place holder for an OnOrbit ID that does not exist in UDL.

Optional place holder for an OnOrbit ID that does not exist in UDL.

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