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 31792U 07029A 25188.57655815 .00000372 00000-0 22577-3 0 9994
2 31792 70.9409 357.8702 0005453 249.2384 110.8153 14.12877676929473
| Epoch (UTC): | 07 July 2025 13:50:14 |
| Eccentricity: | 0.0005453 |
| inclination: | 70.9409° |
| perigee height: | 845 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 357.8702° |
| argument of perigee: | 249.2384° |
| revolutions per day: | 14.12877676 |
| mean anomaly at epoch: | 110.8153° |
| orbit number at epoch: | 92947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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