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 28897U 05043H 23083.59408462 .00005227 00000-0 96358-3 0 9990
2 28897 98.1350 217.3514 0014919 332.4733 160.2953 14.65870058921130
Epoch (UTC): | 24 March 2023 14:15:28 |
Eccentricity: | 0.0014919 |
inclination: | 98.1350° |
perigee height: | 664 km |
apogee height: | 685 km |
right ascension of ascending node: | 217.3514° |
argument of perigee: | 332.4733° |
revolutions per day: | 14.65870058 |
mean anomaly at epoch: | 160.2953° |
orbit number at epoch: | 92113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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