75 lines
1.5 KiB
Plaintext
75 lines
1.5 KiB
Plaintext
"Mars Odyssey" "Sol/Mars"
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{
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Class "spacecraft"
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Mesh "marsodyssey.3ds"
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Radius 0.01
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Beginning "2001 10 24"
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#Ending 2047?
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# Orbital elements are only very approximately correct
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# after completion of aerobraking phase. These were taken
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# from the Mars Odyssey PIP, and only reflect the planned,
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# and not the actual final orbit. A better source would be
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# appreciated.
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EllipticalOrbit
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{
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Epoch 2452251.70833
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Period 0.0822
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SemiMajorAxis 3797.2
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Eccentricity 0.0
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Inclination 93.1
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AscendingNode 35
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ArgOfPericenter 0.0
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MeanAnomaly 0.0
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}
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InfoURL "https://en.wikipedia.org/wiki/2001_Mars_Odyssey"
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}
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"Mars Global Surveyor:MGS:1996-062A" "Sol/Mars"
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{
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Class "spacecraft"
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Mesh "marsglobalsurvr.3ds"
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Radius 0.01
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Beginning "1997 09 11 01:17"
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# Ending 2047?
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# http://mars.jpl.nasa.gov/mgs/status/nav/orbparam-peri2.txt
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EllipticalOrbit
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{
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Epoch 2451973.25864 # 2001 Mar 04 18:12:26
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Period 0.08127579
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SemiMajorAxis 3767.968213
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Eccentricity 0.005809
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Inclination 93.0092
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AscendingNode 28.452982
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ArgOfPericenter 267.202961
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MeanAnomaly 0.0
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}
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FixedRotation { }
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BodyFrame
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{
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TwoVector
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{
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Center "Sol/Mars/Mars Global Surveyor"
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Primary
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{
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Axis "y"
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RelativePosition
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{
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Observer "Sol/Mars/Mars Global Surveyor"
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Target "Sol/Mars"
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}
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}
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Secondary
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{
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Axis "x"
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RelativeVelocity
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{
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Observer "Sol/Mars/Mars Global Surveyor"
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Target "Sol/Mars"
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}
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}
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}
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}
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Albedo 0.3
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InfoURL "https://en.wikipedia.org/wiki/Mars_Global_Surveyor"
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}
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