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 21903U 92012B 21059.40460689 -.00000065 00000-0 -84220-4 0 9996
2 21903 82.9331 262.0510 0041614 284.0317 124.5152 13.74518250453064
Epoch (UTC): | 28 February 2021 09:42:38 |
Eccentricity: | 0.0041614 |
inclination: | 82.9331° |
perigee height: | 953 km |
apogee height: | 1014 km |
right ascension of ascending node: | 262.0510° |
argument of perigee: | 284.0317° |
revolutions per day: | 13.74518250 |
mean anomaly at epoch: | 124.5152° |
orbit number at epoch: | 45306 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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