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 38137U 99025EQJ 24339.36246168 .00000985 00000-0 62547-3 0 9993
2 38137 98.9122 23.1018 0046376 35.1750 325.2464 14.05645098584620
| Epoch (UTC): | 04 December 2024 08:41:56 |
| Eccentricity: | 0.0046376 |
| inclination: | 98.9122° |
| perigee height: | 840 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 23.1018° |
| argument of perigee: | 35.1750° |
| revolutions per day: | 14.05645098 |
| mean anomaly at epoch: | 325.2464° |
| orbit number at epoch: | 58462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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