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 65694U 26145.63918370 +.00000000 +00000-0 +47587-2 0 00001
2 65694 53.1592 348.3381 0003336 96.8535 263.2845 15.30080033 01
| Epoch (UTC): | 25 May 2026 15:20:25 |
| Eccentricity: | 0.0003336 |
| inclination: | 53.1592° |
| perigee height: | 473 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 348.3381° |
| argument of perigee: | 96.8535° |
| revolutions per day: | 15.30080033 |
| mean anomaly at epoch: | 263.2845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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