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 25168.29757468 .00001452 00000-0 76062-3 0 9993
2 11 32.8682 25.5281 1448481 141.3057 230.0783 11.89875246833724
| Epoch (UTC): | 17 June 2025 07:08:30 |
| Eccentricity: | 0.1448481 |
| inclination: | 32.8682° |
| perigee height: | 552 km |
| apogee height: | 2900 km |
| right ascension of ascending node: | 25.5281° |
| argument of perigee: | 141.3057° |
| revolutions per day: | 11.89875246 |
| mean anomaly at epoch: | 230.0783° |
| orbit number at epoch: | 83372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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