View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 41310U 16005A 23028.84143140 .00000062 00000-0 00000-0 0 9999
2 41310 0.0217 46.9063 0004889 233.6664 159.1345 1.00270249 25727
Epoch (UTC): | 28 January 2023 20:11:39 |
Eccentricity: | 0.0004889 |
inclination: | 0.0217° |
perigee height: | 35766 km |
apogee height: | 35807 km |
right ascension of ascending node: | 46.9063° |
argument of perigee: | 233.6664° |
revolutions per day: | 1.00270249 |
mean anomaly at epoch: | 159.1345° |
orbit number at epoch: | 2572 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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