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 32953U 08025A 22179.72672465 .00000024 00000-0 10000-3 0 9997
2 32953 82.5028 176.9256 0018066 233.8044 126.1369 12.43111331639736
Epoch (UTC): | 28 June 2022 17:26:29 |
Eccentricity: | 0.0018066 |
inclination: | 82.5028° |
perigee height: | 1479 km |
apogee height: | 1507 km |
right ascension of ascending node: | 176.9256° |
argument of perigee: | 233.8044° |
revolutions per day: | 12.43111331 |
mean anomaly at epoch: | 126.1369° |
orbit number at epoch: | 63973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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