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 22888U 93070A 23272.54793633 .00000086 00000-0 73076-4 0 9994
2 22888 82.9464 95.1024 0049433 75.0803 339.3470 13.75020516497740
Epoch (UTC): | 29 September 2023 13:09:01 |
Eccentricity: | 0.0049433 |
inclination: | 82.9464° |
perigee height: | 945 km |
apogee height: | 1018 km |
right ascension of ascending node: | 95.1024° |
argument of perigee: | 75.0803° |
revolutions per day: | 13.75020516 |
mean anomaly at epoch: | 339.3470° |
orbit number at epoch: | 49774 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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