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 42120U 81053QG 24355.21851850 .00001340 00000-0 16534-2 0 9994
2 42120 82.9283 78.2359 0191770 39.3865 322.1046 13.57074353547558
| Epoch (UTC): | 20 December 2024 05:14:39 |
| Eccentricity: | 0.0191770 |
| inclination: | 82.9283° |
| perigee height: | 904 km |
| apogee height: | 1189 km |
| right ascension of ascending node: | 78.2359° |
| argument of perigee: | 39.3865° |
| revolutions per day: | 13.57074353 |
| mean anomaly at epoch: | 322.1046° |
| orbit number at epoch: | 54755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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