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 20692U 26040.75029138 +.00000000 +00000-0 +42480-3 0 00000
2 20692 63.2946 194.0929 0878416 82.2236 287.7509 13.63162136 02
| Epoch (UTC): | 09 February 2026 18:00:25 |
| Eccentricity: | 0.0878416 |
| inclination: | 63.2946° |
| perigee height: | 374 km |
| apogee height: | 1674 km |
| right ascension of ascending node: | 194.0929° |
| argument of perigee: | 82.2236° |
| revolutions per day: | 13.63162136 |
| mean anomaly at epoch: | 287.7509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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