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 43131U 18004W 23088.76662641 .01082452 54979-3 27529-2 0 9990
2 43131 97.3256 178.5027 0008034 280.7423 79.2948 15.95484049290736
Epoch (UTC): | 29 March 2023 18:23:56 |
Eccentricity: | 0.0008034 |
inclination: | 97.3256° |
perigee height: | 281 km |
apogee height: | 292 km |
right ascension of ascending node: | 178.5027° |
argument of perigee: | 280.7423° |
revolutions per day: | 15.95484049 |
mean anomaly at epoch: | 79.2948° |
orbit number at epoch: | 29073 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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