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 25339.94478439 .00001799 00000-0 10429-2 0 9992
2 00012 32.8950 186.2566 1647157 161.8380 204.8902 11.48370539509105
| Epoch (UTC): | 05 December 2025 22:40:29 |
| Eccentricity: | 0.1647157 |
| inclination: | 32.8950° |
| perigee height: | 554 km |
| apogee height: | 3287 km |
| right ascension of ascending node: | 186.2566° |
| argument of perigee: | 161.8380° |
| revolutions per day: | 11.48370539 |
| mean anomaly at epoch: | 204.8902° |
| orbit number at epoch: | 50910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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