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 00115U 60002D 25340.01346523 .00005977 00000-0 53572-3 0 9996
2 00115 48.1632 330.2459 0026554 107.4031 252.9793 14.96615345489188
| Epoch (UTC): | 06 December 2025 00:19:23 |
| Eccentricity: | 0.0026554 |
| inclination: | 48.1632° |
| perigee height: | 559 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 330.2459° |
| argument of perigee: | 107.4031° |
| revolutions per day: | 14.96615345 |
| mean anomaly at epoch: | 252.9793° |
| orbit number at epoch: | 48918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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