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 data is extracted from the following two-line orbital elements,
1 11U 59001A 25131.52786303 .00001735 00000-0 89775-3 0 9998
2 11 32.8731 164.5524 1449114 292.2443 53.0924 11.89754138829341
| Epoch (UTC): | 11 May 2025 12:40:07 |
| Eccentricity: | 0.1449114 |
| inclination: | 32.8731° |
| perigee height: | 552 km |
| apogee height: | 2901 km |
| right ascension of ascending node: | 164.5524° |
| argument of perigee: | 292.2443° |
| revolutions per day: | 11.89754138 |
| mean anomaly at epoch: | 53.0924° |
| orbit number at epoch: | 82934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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