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 37841U 11058D 24357.63797003 .00000605 00000-0 18563-3 0 9991
2 37841 19.9717 96.7994 0011859 7.4286 120.2062 14.11315557681218
| Epoch (UTC): | 22 December 2024 15:18:40 |
| Eccentricity: | 0.0011859 |
| inclination: | 19.9717° |
| perigee height: | 846 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 96.7994° |
| argument of perigee: | 7.4286° |
| revolutions per day: | 14.11315557 |
| mean anomaly at epoch: | 120.2062° |
| orbit number at epoch: | 68121 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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