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 is defined by the following mean orbital elements,
1 36795U 26032.52729711 +.00000000 +00000-0 +16613-3 0 00000
2 36795 97.7783 84.8880 0010320 272.6223 87.3807 14.78727886 00
| Epoch (UTC): | 01 February 2026 12:39:18 |
| Eccentricity: | 0.0010320 |
| inclination: | 97.7783° |
| perigee height: | 626 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 84.8880° |
| argument of perigee: | 272.6223° |
| revolutions per day: | 14.78727886 |
| mean anomaly at epoch: | 87.3807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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