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Telemachus Reborn API
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Schema
Checked 2h ago · Updated 2mo ago
Details
Filter operations
alarm
4
astrogator
15
body
41
career
4
comms
5
deltav
26
docking
5
far
17
fbw
7
flight
58
landing
8
maneuver
15
map
4
mechjeb
18
navigation
12
orbit
73
get
Ascending Node Vector
get
Apoapsis Altitude
get
Apoapsis Radius
get
Argument of Periapsis
get
Closest Encounter Body Name
get
Closest Target Approach UT
get
Eccentric Anomaly
get
Eccentricity
get
Eccentricity Vector
get
Encounter/Escape Body Name
get
SOI Encounter Exists (-1=escape, 0=none, 1=encounter)
get
Time Until SOI Encounter/Escape
get
Orbit Patch End UT
get
Epoch
get
Language
get
Specific Angular Momentum Vector
get
Inclination
get
Longitude of Ascending Node
get
Mean Anomaly at Epoch
get
Anomalistic Period (Principia)
get
Mean Apoapsis Altitude (Principia)
get
Mean Apoapsis Altitude Range (Principia)
get
Mean Argument of Periapsis (Principia)
get
Mean Eccentricity (Principia)
get
Mean Eccentricity Range (Principia)
get
Mean Inclination (Principia)
get
Mean Inclination Range (Principia)
get
Mean Longitude of Ascending Node (Principia)
get
Nodal Period (Principia)
get
Nodal Precession Rate (rad/s, Principia)
get
Mean Periapsis Altitude (Principia)
get
Mean Periapsis Altitude Range (Principia)
get
Orbit Recurrence Info (Principia)
get
Sidereal Period (Principia)
get
Mean Semimajor Axis (Principia)
get
Mean SMA Range {min,max} (Principia)
get
Mean Anomaly
get
Next Apsis Type (-1=Pe, 1=Ap, 0=N/A)
get
Specific Orbital Energy
get
Orbital Speed
get
Orbital Speed at Orbit Time
get
Orbital Speed at Distance
get
Orbit Normal Vector
get
Detailed Orbit Patches Info
get
Orbit Percent
get
Patch End Transition Type
get
Patch Start Transition Type
get
Periapsis Altitude
get
Periapsis Radius
get
Orbital Period
get
Orbital Position Vector
get
Orbital Radius
get
Radius at True Anomaly
get
Reference Body Name
get
The orbit patch's predicted displacement from the center of the main body at the given true anomaly
get
The orbit patch's predicted displacement from the center of the main body at the given universal time
get
Relative Velocity
get
Semi-latus Rectum
get
Semi-minor Axis
get
Semimajor Axis
get
Orbit Patch Start UT
get
Time of Periapsis Passage
get
Time to Apoapsis
get
Time to Next Apsis
get
Time to Periapsis
get
Time to Transition 1
get
Time to Transition 2
get
True Anomaly
get
True Anomaly at Radius
get
The orbit patch's True Anomaly at Universal Time
get
The orbit patch's Universal Time at True Anomaly
get
UT of SOI Transition
get
Orbital Velocity Vector
principia
10
realchute
9
resource
5
science
3
sensor
5
system
8
target
31
thermal
12
timewarp
7
vessel
84
orbit
Eccentricity Vector
get
/api/o.eccVec
Response
Successful response
object
required
o.eccVec
number[]
Changes