
Initially goal is to include the above 8. Then we can expand to defunct ones and then even probes of all other planets.
If I understood the process correctly, there are two steps -
-Find the orbital elements around the orbiting planet.
-Find/create 3d models
This is the result so far(only first five orbits, haven’t added models yet) :
Orbital Elements
For all the NASA probes,
I used NASA horizons : https://ssd.jpl.nasa.gov/horizons.cgi#top
I don’t know if the procedure I’m using is correct, would really appreciate if someone takes a look : Sorry for the robovoice, something is wrong with my mic!
[spoiler][/font]
Im using the starlink model by mosfet temporarily
Spacecraft "2001 Mars Odyssey"
{
Model "spacecraft/starlink2.sss"
NoLighting true
ParentBody "Mars"
Radius 0.005
Orbit
{
Epoch 2459470.500000000
SemiMajorAxisKm 3.804825638151244E+03
PeriodDays 8.247123034000406E-02
MeanAnomaly +2.671359404812213E+02
ArgOfPericenter 2.647507108749190E+02
Eccentricity 7.800466241880192E-03
Inclination 9.303648630846963E+01
AscendingNode 2.458432599208940E+02
RefPlane "Equator"
}
}
Spacecraft "Mars Express"
{
Model "spacecraft/starlink2.sss"
NoLighting true
ParentBody "Mars"
Radius 0.005
Orbit
{
Epoch 2459470.500000000
SemiMajorAxisKm 8.816622223094781E+03
PeriodDays 2.909066728059267E-01
MeanAnomaly +1.159532962125450E+02
ArgOfPericenter 8.850124302639026E+01
Eccentricity 5.722803295382805E-01
Inclination 8.703557228206786E+01
AscendingNode 1.566587940166173E+02
RefPlane "Equator"
}
}
Spacecraft "Mars Reconnaissance Orbiter"
{
Model "spacecraft/starlink2.sss"
NoLighting true
ParentBody "Mars"
Radius 0.005
Orbit
{
Epoch 2459470.500000000
SemiMajorAxisKm 3.656402300141111E+03
PeriodDays 7.769289326216809E-02
MeanAnomaly +2.100756546089188E+02
ArgOfPericenter 2.815948883696823E+02
Eccentricity 9.050006486433003E-03
Inclination 9.241127975856789E+01
AscendingNode 1.736126156594644E+01
RefPlane "Equator"
}
}
Spacecraft "Mars Orbiter Mission (Mangalyaan)"
{
Model "spacecraft/starlink2.sss"
NoLighting true
ParentBody "Mars"
Radius 0.005
Orbit
{
Epoch 2459470.500000000
SemiMajorAxisKm 3.975242095536460E+04
PeriodDays 2.785131521643801E+00
MeanAnomaly +2.389013043061660E+02
ArgOfPericenter 1.718757535681395E+02
Eccentricity 9.009581874687916E-01
Inclination 1.538160153039837E+02
AscendingNode 2.520703732771788E+02
RefPlane "Equator"
}
}
Spacecraft "MAVEN"
{
Model "spacecraft/starlink2.sss"
NoLighting true
ParentBody "Mars"
Radius 0.005
Orbit
{
Epoch 2459470.500000000
SemiMajorAxisKm 5.676638613432664E+03
PeriodDays 1.502924641523433E-01
MeanAnomaly +1.842196155038370E+02
ArgOfPericenter 3.187312489201630E+01
Eccentricity 3.657911727466540E-01
Inclination 7.486214508328472E+01
AscendingNode 2.607542977538328E+02
RefPlane "Equator"
}
}
[/spoiler]
So far, this is what I have found for Tiawen-1

https://en.wikipedia.org/wiki/Tianwen-1#Orbital_elements
ExoMars - Thanks to ChrisGnam on reddit :https://www.reddit.com/r/space/comments/pmxnod/all_space_questions_thread_for_week_of_september/hcowy2r/?context=3
Yet to find values for Emirates Mars mission.
3d models - needs some work to convert formats. I am currently checking Harbinger Dawn’s tutorial for this.
If anyone wants to try converting, here are some links I found so far :
2001 Mars Odyssey -https://nasa3d.arc.nasa.gov/detail/eoss-marsodyssey
Mars Express - https://sketchfab.com/3d-models/mars-ex ... cb3ee40a89
(have to check license)
Mars Reconnaissance Orbiter-https://nasa3d.arc.nasa.gov/search/Mars%20Reconnaissance%20Orbiter/
Mars Orbiter Mission -https://sketchfab.com/3d-models/mars-orbiter-mission-mangalyana-by-isro-72a4112ce14d4ce3887a8a149f5589b7(have to check license)
Maven -https://nasa3d.arc.nasa.gov/detail/maven-jpl
ExoMars Trace Gas Orbiter -https://solarsystem.nasa.gov/resources/2350/trace-gas-orbiter-3d-model/
Emirates Mars Mission - ???
Taiwen 1 - ???