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 42188U 81053TC 24357.98852817 .00005178 00000-0 27646-2 0 9997
2 42188 82.8505 200.6882 0055217 284.9796 74.5272 14.12316697215627
| Epoch (UTC): | 22 December 2024 23:43:28 |
| Eccentricity: | 0.0055217 |
| inclination: | 82.8505° |
| perigee height: | 811 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 200.6882° |
| argument of perigee: | 284.9796° |
| revolutions per day: | 14.12316697 |
| mean anomaly at epoch: | 74.5272° |
| orbit number at epoch: | 21562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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