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 20691U 26046.77350406 +.00000000 +00000-0 +26884-3 0 00002
2 20691 63.2945 179.1111 0883226 82.8337 287.2151 13.61817088 09
| Epoch (UTC): | 15 February 2026 18:33:50 |
| Eccentricity: | 0.0883226 |
| inclination: | 63.2945° |
| perigee height: | 375 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 179.1111° |
| argument of perigee: | 82.8337° |
| revolutions per day: | 13.61817088 |
| mean anomaly at epoch: | 287.2151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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