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Time tag for navigation data:
15 December 1997, 12:00:00 PST |
New - Detailed History of Orbital Parameters
Surveyor was launched on 7 November 1996 at 12:00:50 EST. The spaecraft
is currently in an orbit around Mars. Currently, radio signals sent from
Surveyor take 17 minutes, 19 seconds to reach Earth.
Distance from Earth |
311.66 million kilometers |
Earth Relative Velocity |
49.45 km per second |
Declination |
-21.74 degrees |
Right Ascention |
300.50 degrees |
Distance from Sun |
207.20 million kilometers |
Sun Relative Velocity |
26.44 km per second |
Capture Orbit Information
The following table contains osculating orbital elements as measured at
the first apoapsis (high point of the orbit) after Mars orbit insertion.
Epoch
9/12/97 23:58:53.4 UTC (JD 2450704.499229)
Coordinate Frame
Mars Mean Equator of Date (plane)
IAU Vector of Epoch J2000 (X-axis)
Semi-major Axis |
30531.953 km |
Period |
44.9928 hours |
Eccentricity |
0.880473 |
True Anomaly |
180 deg. |
Mean Anomaly |
180 deg. |
Long. Ascn. Node |
-40.506 deg. |
Arg. of Pericenter |
148.568 deg. |
Inclination |
93.259 deg. |
Apopasis Radius |
57414.5 km |
Apoapsis Velocity |
0.298599 km/s |
Periapsis Radius |
3651.4 km |
Periapsis Velocity |
4.696989 km/s |
Related Quantities
The following parameters are relevant to the generation of the orbital elements
listed above.
GM Mars |
42828.314 km^3/s^2 |
GM Sun |
132712440018 km^3/s^2 |
Mars Equatorial Radius |
3394.5 x 3399.2 km |
Mars Polar Radius |
3376.1 km |
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