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 65866U 26145.40635411 +.00000000 +00000-0 +67867-3 0 00003
2 65866 53.1604 297.6687 0001621 81.8504 278.2682 15.34406889 06
| Epoch (UTC): | 25 May 2026 09:45:08 |
| Eccentricity: | 0.0001621 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 297.6687° |
| argument of perigee: | 81.8504° |
| revolutions per day: | 15.34406889 |
| mean anomaly at epoch: | 278.2682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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