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 42200U 81053TQ 23336.78761194 .00004257 00000-0 27190-2 0 9994
2 42200 82.9832 130.1502 0071888 6.6635 353.5474 14.02023790511390
Epoch (UTC): | 02 December 2023 18:54:09 |
Eccentricity: | 0.0071888 |
inclination: | 82.9832° |
perigee height: | 834 km |
apogee height: | 939 km |
right ascension of ascending node: | 130.1502° |
argument of perigee: | 6.6635° |
revolutions per day: | 14.02023790 |
mean anomaly at epoch: | 353.5474° |
orbit number at epoch: | 51139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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