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 36794U 26066.90660118 +.00000000 +00000-0 +15013-2 0 00005
2 36794 49.5024 294.0642 5434282 66.4810 340.4861 4.93733369 08
| Epoch (UTC): | 07 March 2026 21:45:30 |
| Eccentricity: | 0.5434282 |
| inclination: | 49.5024° |
| perigee height: | 273 km |
| apogee height: | 16107 km |
| right ascension of ascending node: | 294.0642° |
| argument of perigee: | 66.4810° |
| revolutions per day: | 4.93733369 |
| mean anomaly at epoch: | 340.4861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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