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 36799U 10035E 25346.25189515 .00026444 00000-0 11105-2 0 9999
2 36799 98.0592 272.6056 0003349 133.5881 226.5632 15.23428174839165
| Epoch (UTC): | 12 December 2025 06:02:43 |
| Eccentricity: | 0.0003349 |
| inclination: | 98.0592° |
| perigee height: | 493 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 272.6056° |
| argument of perigee: | 133.5881° |
| revolutions per day: | 15.23428174 |
| mean anomaly at epoch: | 226.5632° |
| orbit number at epoch: | 83916 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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