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 26071.96860558 +.00000000 +00000-0 +15225-2 0 00002
2 36794 49.5014 290.3881 5433136 69.6086 339.2034 4.93869424 08
| Epoch (UTC): | 12 March 2026 23:14:47 |
| Eccentricity: | 0.5433136 |
| inclination: | 49.5014° |
| perigee height: | 274 km |
| apogee height: | 16101 km |
| right ascension of ascending node: | 290.3881° |
| argument of perigee: | 69.6086° |
| revolutions per day: | 4.93869424 |
| mean anomaly at epoch: | 339.2034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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