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 115U 60002D 25343.61853389 .00005961 00000-0 53374-3 0 9991
2 115 48.1635 312.5525 0026688 124.0194 236.3264 14.96659867489727
| Epoch (UTC): | 09 December 2025 14:50:41 |
| Eccentricity: | 0.0026688 |
| inclination: | 48.1635° |
| perigee height: | 558 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 312.5525° |
| argument of perigee: | 124.0194° |
| revolutions per day: | 14.96659867 |
| mean anomaly at epoch: | 236.3264° |
| orbit number at epoch: | 48972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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