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 is defined by the following mean orbital elements,
1 36125U 09073B 25257.90654500 0.00000800 00000-0 10667-3 0 00
2 36125 98.0279 348.8392 0024474 340.9019 19.0980 14.79484727 08
| Epoch (UTC): | 14 September 2025 21:45:25 |
| Eccentricity: | 0.0024474 |
| inclination: | 98.0279° |
| perigee height: | 614 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 348.8392° |
| argument of perigee: | 340.9019° |
| revolutions per day: | 14.79484727 |
| mean anomaly at epoch: | 19.0980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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