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 22207U 92073A 23272.21500324 .00000101 00000-0 93367-4 0 9991
2 22207 82.9224 150.1498 0031360 236.6851 242.4700 13.72949920548815
Epoch (UTC): | 29 September 2023 05:09:36 |
Eccentricity: | 0.0031360 |
inclination: | 82.9224° |
perigee height: | 966 km |
apogee height: | 1012 km |
right ascension of ascending node: | 150.1498° |
argument of perigee: | 236.6851° |
revolutions per day: | 13.72949920 |
mean anomaly at epoch: | 242.4700° |
orbit number at epoch: | 54881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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