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 59U 60013B 25344.79814905 .00000135 00000-0 59258-4 0 9997
2 59 28.2503 11.5363 0188898 174.1198 186.1614 13.53154694217635
| Epoch (UTC): | 10 December 2025 19:09:20 |
| Eccentricity: | 0.0188898 |
| inclination: | 28.2503° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 11.5363° |
| argument of perigee: | 174.1198° |
| revolutions per day: | 13.53154694 |
| mean anomaly at epoch: | 186.1614° |
| orbit number at epoch: | 21763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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