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 42836U 17042M 23083.55692439 .00009754 00000-0 92336-3 0 9997
2 42836 97.3946 287.0629 0013232 145.2939 214.9147 14.93753564309929
Epoch (UTC): | 24 March 2023 13:21:58 |
Eccentricity: | 0.0013232 |
inclination: | 97.3946° |
perigee height: | 577 km |
apogee height: | 595 km |
right ascension of ascending node: | 287.0629° |
argument of perigee: | 145.2939° |
revolutions per day: | 14.93753564 |
mean anomaly at epoch: | 214.9147° |
orbit number at epoch: | 30992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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