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 36796U 10035B 23083.49442453 .00008929 00000-0 91714-3 0 9994
2 36796 98.2161 283.7451 0011179 306.7306 53.2883 14.90578142688578
Epoch (UTC): | 24 March 2023 11:51:58 |
Eccentricity: | 0.0011179 |
inclination: | 98.2161° |
perigee height: | 588 km |
apogee height: | 604 km |
right ascension of ascending node: | 283.7451° |
argument of perigee: | 306.7306° |
revolutions per day: | 14.90578142 |
mean anomaly at epoch: | 53.2883° |
orbit number at epoch: | 68857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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