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 65501U 26145.09676898 +.00000000 +00000-0 +10610-2 0 00001
2 65501 53.1596 275.0106 0001291 97.9629 262.1520 15.34389043 02
| Epoch (UTC): | 25 May 2026 02:19:20 |
| Eccentricity: | 0.0001291 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 275.0106° |
| argument of perigee: | 97.9629° |
| revolutions per day: | 15.34389043 |
| mean anomaly at epoch: | 262.1520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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