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 00012U 59001B 25340.64021673 .00001863 00000-0 10797-2 0 9995
2 00012 32.8951 183.8057 1647152 165.5216 199.9042 11.48373302509186
| Epoch (UTC): | 06 December 2025 15:21:54 |
| Eccentricity: | 0.1647152 |
| inclination: | 32.8951° |
| perigee height: | 553 km |
| apogee height: | 3287 km |
| right ascension of ascending node: | 183.8057° |
| argument of perigee: | 165.5216° |
| revolutions per day: | 11.48373302 |
| mean anomaly at epoch: | 199.9042° |
| orbit number at epoch: | 50918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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