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 26064.88139479 +.00000000 +00000-0 +14195-2 0 00001
2 36794 49.5045 295.5363 5434643 65.2286 340.9788 4.93685592 09
| Epoch (UTC): | 05 March 2026 21:09:12 |
| Eccentricity: | 0.5434643 |
| inclination: | 49.5045° |
| perigee height: | 273 km |
| apogee height: | 16109 km |
| right ascension of ascending node: | 295.5363° |
| argument of perigee: | 65.2286° |
| revolutions per day: | 4.93685592 |
| mean anomaly at epoch: | 340.9788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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