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 22178.51948508 .00000024 00000-0 10000-3 0 9997
2 32953 82.5028 177.6763 0018054 236.3868 123.5490 12.43111272639589
Epoch (UTC): | 27 June 2022 12:28:03 |
Eccentricity: | 0.0018054 |
inclination: | 82.5028° |
perigee height: | 1479 km |
apogee height: | 1507 km |
right ascension of ascending node: | 177.6763° |
argument of perigee: | 236.3868° |
revolutions per day: | 12.43111272 |
mean anomaly at epoch: | 123.5490° |
orbit number at epoch: | 63958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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