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 21398U 91039B 22226.62817777 .00000189 00000-0 21860-4 0 9993
2 21398 82.5210 271.7365 0022702 122.9943 237.3457 14.79945503682584
Epoch (UTC): | 14 August 2022 15:04:34 |
Eccentricity: | 0.0022702 |
inclination: | 82.5210° |
perigee height: | 613 km |
apogee height: | 645 km |
right ascension of ascending node: | 271.7365° |
argument of perigee: | 122.9943° |
revolutions per day: | 14.79945503 |
mean anomaly at epoch: | 237.3457° |
orbit number at epoch: | 68258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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