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 31793U 07029B 25193.83443510 .00000289 00000-0 17458-3 0 9996
2 31793 70.9772 316.5562 0002119 280.4231 247.7317 14.14790292931449
| Epoch (UTC): | 12 July 2025 20:01:35 |
| Eccentricity: | 0.0002119 |
| inclination: | 70.9772° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 316.5562° |
| argument of perigee: | 280.4231° |
| revolutions per day: | 14.14790292 |
| mean anomaly at epoch: | 247.7317° |
| orbit number at epoch: | 93144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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