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 51975U 26144.97227821 +.00000000 +00000-0 -18257-5 0 00004
2 51975 53.1614 29.0264 0001279 94.0629 266.0519 15.31701254 09
| Epoch (UTC): | 24 May 2026 23:20:04 |
| Eccentricity: | 0.0001279 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 29.0264° |
| argument of perigee: | 94.0629° |
| revolutions per day: | 15.31701254 |
| mean anomaly at epoch: | 266.0519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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