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 65693U 26144.95339610 +.00000000 +00000-0 +39014-3 0 00005
2 65693 53.1596 341.1781 0001134 85.0361 275.0770 15.30211613 08
| Epoch (UTC): | 24 May 2026 22:52:53 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 341.1781° |
| argument of perigee: | 85.0361° |
| revolutions per day: | 15.30211613 |
| mean anomaly at epoch: | 275.0770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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