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 65863U 26145.40004328 +.00000000 +00000-0 +95464-3 0 00001
2 65863 53.1595 297.6332 0002092 87.5716 272.5526 15.34421610 03
| Epoch (UTC): | 25 May 2026 09:36:03 |
| Eccentricity: | 0.0002092 |
| inclination: | 53.1595° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 297.6332° |
| argument of perigee: | 87.5716° |
| revolutions per day: | 15.34421610 |
| mean anomaly at epoch: | 272.5526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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