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 36148U 99025DRV 24355.39392785 .00011581 00000-0 80371-2 0 9999
2 36148 98.3967 237.5146 0294869 249.2963 107.6358 13.80131349853051
| Epoch (UTC): | 20 December 2024 09:27:15 |
| Eccentricity: | 0.0294869 |
| inclination: | 98.3967° |
| perigee height: | 747 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 237.5146° |
| argument of perigee: | 249.2963° |
| revolutions per day: | 13.80131349 |
| mean anomaly at epoch: | 107.6358° |
| orbit number at epoch: | 85305 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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