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 26158.93918453 +.00000000 +00000-0 +24620-3 0 00002
2 20691 63.2937 236.7595 0880665 84.9980 285.0873 13.62735939 09
| Epoch (UTC): | 07 June 2026 22:32:25 |
| Eccentricity: | 0.0880665 |
| inclination: | 63.2937° |
| perigee height: | 374 km |
| apogee height: | 1678 km |
| right ascension of ascending node: | 236.7595° |
| argument of perigee: | 84.9980° |
| revolutions per day: | 13.62735939 |
| mean anomaly at epoch: | 285.0873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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