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 28096U 03054B 21016.72145103 0.00000000 00000-0 00000-0 0 03
2 28096 63.6872 348.3858 0217190 222.8034 137.1966 13.40864869 01
Epoch (UTC): | 16 January 2021 17:18:53 |
Eccentricity: | 0.0217190 |
inclination: | 63.6872° |
perigee height: | 943 km |
apogee height: | 1268 km |
right ascension of ascending node: | 348.3858° |
argument of perigee: | 222.8034° |
revolutions per day: | 13.40864869 |
mean anomaly at epoch: | 137.1966° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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