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 20641U 26145.27769839 +.00000000 +00000-0 +00000-0 0 00005
2 20641 63.3916 95.6738 4062026 266.2880 47.7388 6.02596284 02
| Epoch (UTC): | 25 May 2026 06:39:53 |
| Eccentricity: | 0.4062026 |
| inclination: | 63.3916° |
| perigee height: | 1196 km |
| apogee height: | 11560 km |
| right ascension of ascending node: | 95.6738° |
| argument of perigee: | 266.2880° |
| revolutions per day: | 6.02596284 |
| mean anomaly at epoch: | 47.7388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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