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 28893U 05043D 23088.34548351 .00001070 00000-0 22254-3 0 9992
2 28893 98.1395 212.1352 0015031 4.8029 355.3314 14.62011418928579
Epoch (UTC): | 29 March 2023 08:17:29 |
Eccentricity: | 0.0015031 |
inclination: | 98.1395° |
perigee height: | 676 km |
apogee height: | 697 km |
right ascension of ascending node: | 212.1352° |
argument of perigee: | 4.8029° |
revolutions per day: | 14.62011418 |
mean anomaly at epoch: | 355.3314° |
orbit number at epoch: | 92857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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