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 13807U 81053HB 22222.06566981 .00001299 00000-0 61738-3 0 9996
2 13807 82.9519 75.9062 0012550 1.4674 358.6541 14.18728193779312
Epoch (UTC): | 10 August 2022 01:34:33 |
Eccentricity: | 0.0012550 |
inclination: | 82.9519° |
perigee height: | 820 km |
apogee height: | 839 km |
right ascension of ascending node: | 75.9062° |
argument of perigee: | 1.4674° |
revolutions per day: | 14.18728193 |
mean anomaly at epoch: | 358.6541° |
orbit number at epoch: | 77931 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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