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 28895U 05043F 23272.30463462 .00002585 00000-0 47857-3 0 9992
2 28895 98.1679 43.6760 0017290 103.7570 256.5559 14.66093371956065
Epoch (UTC): | 29 September 2023 07:18:40 |
Eccentricity: | 0.0017290 |
inclination: | 98.1679° |
perigee height: | 661 km |
apogee height: | 686 km |
right ascension of ascending node: | 43.6760° |
argument of perigee: | 103.7570° |
revolutions per day: | 14.66093371 |
mean anomaly at epoch: | 256.5559° |
orbit number at epoch: | 95606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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