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 65391U 26145.39090664 +.00000000 +00000-0 +22436-3 0 00002
2 65391 97.4539 16.7920 0001917 71.1039 289.0396 15.05656727 08
| Epoch (UTC): | 25 May 2026 09:22:54 |
| Eccentricity: | 0.0001917 |
| inclination: | 97.4539° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.7920° |
| argument of perigee: | 71.1039° |
| revolutions per day: | 15.05656727 |
| mean anomaly at epoch: | 289.0396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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