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 26066.09654363 +.00000000 +00000-0 +13719-2 0 00001
2 36794 49.5037 294.6546 5434447 65.9793 340.6851 4.93713027 08
| Epoch (UTC): | 07 March 2026 02:19:01 |
| Eccentricity: | 0.5434447 |
| inclination: | 49.5037° |
| perigee height: | 273 km |
| apogee height: | 16108 km |
| right ascension of ascending node: | 294.6546° |
| argument of perigee: | 65.9793° |
| revolutions per day: | 4.93713027 |
| mean anomaly at epoch: | 340.6851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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