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 28538U 05004B 24358.04242528 .00000019 00000-0 16162-3 0 9993
2 28538 63.8223 213.3492 0212761 285.8401 71.9267 13.43305322 32455
Epoch (UTC): | 23 December 2024 01:01:05 |
Eccentricity: | 0.0212761 |
inclination: | 63.8223° |
perigee height: | 938 km |
apogee height: | 1256 km |
right ascension of ascending node: | 213.3492° |
argument of perigee: | 285.8401° |
revolutions per day: | 13.43305322 |
mean anomaly at epoch: | 71.9267° |
orbit number at epoch: | 3245 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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