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 65093U 26145.10175251 +.00000000 +00000-0 +69999-3 0 00001
2 65093 53.1597 29.2635 0001047 99.5889 260.5235 15.42178873 01
| Epoch (UTC): | 25 May 2026 02:26:31 |
| Eccentricity: | 0.0001047 |
| inclination: | 53.1597° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 29.2635° |
| argument of perigee: | 99.5889° |
| revolutions per day: | 15.42178873 |
| mean anomaly at epoch: | 260.5235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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