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 29517U 06048B 25349.09949434 .00000136 00000-0 14990-3 0 9993
2 29517 28.2684 9.7027 4058225 207.8319 122.8694 6.89875492381133
| Epoch (UTC): | 15 December 2025 02:23:16 |
| Eccentricity: | 0.4058225 |
| inclination: | 28.2684° |
| perigee height: | 547 km |
| apogee height: | 10008 km |
| right ascension of ascending node: | 9.7027° |
| argument of perigee: | 207.8319° |
| revolutions per day: | 6.89875492 |
| mean anomaly at epoch: | 122.8694° |
| orbit number at epoch: | 38113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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