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 00011U 59001A 25118.68560254 .00003514 00000-0 18396-2 0 9992
2 00011 32.8722 213.0873 1448707 219.2896 129.3277 11.89695470486076
| Epoch (UTC): | 28 April 2025 16:27:16 |
| Eccentricity: | 0.1448707 |
| inclination: | 32.8722° |
| perigee height: | 553 km |
| apogee height: | 2901 km |
| right ascension of ascending node: | 213.0873° |
| argument of perigee: | 219.2896° |
| revolutions per day: | 11.89695470 |
| mean anomaly at epoch: | 129.3277° |
| orbit number at epoch: | 48607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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