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 21056.85455040 0.00000000 00000-0 00000-0 0 07
2 28541 63.4256 345.1922 0390096 358.4625 1.5375 13.40817317 00
Epoch (UTC): | 25 February 2021 20:30:33 |
Eccentricity: | 0.0390096 |
inclination: | 63.4256° |
perigee height: | 814 km |
apogee height: | 1398 km |
right ascension of ascending node: | 345.1922° |
argument of perigee: | 358.4625° |
revolutions per day: | 13.40817317 |
mean anomaly at epoch: | 1.5375° |
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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