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 42761U 17034D 22144.88797081 .00005482 00000-0 32767-3 0 9993
2 42761 43.0170 101.3796 0008003 149.6976 257.9027 15.11833358272794
Epoch (UTC): | 24 May 2022 21:18:40 |
Eccentricity: | 0.0008003 |
inclination: | 43.0170° |
perigee height: | 525 km |
apogee height: | 536 km |
right ascension of ascending node: | 101.3796° |
argument of perigee: | 149.6976° |
revolutions per day: | 15.11833358 |
mean anomaly at epoch: | 257.9027° |
orbit number at epoch: | 27279 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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