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 65101U 26145.09347574 +.00000000 +00000-0 +62818-3 0 00001
2 65101 53.1600 31.3379 0001179 89.3678 270.7460 15.34393925 05
| Epoch (UTC): | 25 May 2026 02:14:36 |
| Eccentricity: | 0.0001179 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 31.3379° |
| argument of perigee: | 89.3678° |
| revolutions per day: | 15.34393925 |
| mean anomaly at epoch: | 270.7460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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