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 26156.95787593 +.00000000 +00000-0 +27239-3 0 00000
2 20691 63.2940 242.1041 0880742 84.9611 285.1241 13.62722508 05
| Epoch (UTC): | 05 June 2026 22:59:20 |
| Eccentricity: | 0.0880742 |
| inclination: | 63.2940° |
| perigee height: | 374 km |
| apogee height: | 1678 km |
| right ascension of ascending node: | 242.1041° |
| argument of perigee: | 84.9611° |
| revolutions per day: | 13.62722508 |
| mean anomaly at epoch: | 285.1241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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