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 65891U 26145.33062150 +.00000000 +00000-0 +46629-3 0 00000
2 65891 53.1598 15.6922 0001135 92.9711 267.1419 15.30208947 05
| Epoch (UTC): | 25 May 2026 07:56:05 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 15.6922° |
| argument of perigee: | 92.9711° |
| revolutions per day: | 15.30208947 |
| mean anomaly at epoch: | 267.1419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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