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 65894U 26145.37588655 +.00000000 +00000-0 +42754-3 0 00005
2 65894 53.1601 15.2585 0001644 96.2108 263.9081 15.30212648 08
| Epoch (UTC): | 25 May 2026 09:01:16 |
| Eccentricity: | 0.0001644 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 15.2585° |
| argument of perigee: | 96.2108° |
| revolutions per day: | 15.30212648 |
| mean anomaly at epoch: | 263.9081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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