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 28541U 05004C 21014.11935310 0.00000000 00000-0 00000-0 0 03
2 28541 63.4208 94.3263 0382069 358.7214 1.2786 13.40814198 03
Epoch (UTC): | 14 January 2021 02:51:52 |
Eccentricity: | 0.0382069 |
inclination: | 63.4208° |
perigee height: | 820 km |
apogee height: | 1392 km |
right ascension of ascending node: | 94.3263° |
argument of perigee: | 358.7214° |
revolutions per day: | 13.40814198 |
mean anomaly at epoch: | 1.2786° |
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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