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 65829U 26145.27131226 +.00000000 +00000-0 +73203-3 0 00003
2 65829 53.1575 95.1391 0001134 93.9109 266.2021 15.30209563 09
| Epoch (UTC): | 25 May 2026 06:30:41 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.1391° |
| argument of perigee: | 93.9109° |
| revolutions per day: | 15.30209563 |
| mean anomaly at epoch: | 266.2021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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