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 20775U 26037.65358789 +.00000000 +00000-0 +55071-3 0 00004
2 20775 82.9020 279.1988 0367274 117.9812 245.9086 14.88035941 03
| Epoch (UTC): | 06 February 2026 15:41:09 |
| Eccentricity: | 0.0367274 |
| inclination: | 82.9020° |
| perigee height: | 348 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 279.1988° |
| argument of perigee: | 117.9812° |
| revolutions per day: | 14.88035941 |
| mean anomaly at epoch: | 245.9086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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