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 25346.30869573 -.00000050 00000-0 -12373-5 0 9990
2 31793 70.9756 356.0640 0002189 262.4289 108.4804 14.14814824953016
| Epoch (UTC): | 12 December 2025 07:24:31 |
| Eccentricity: | 0.0002189 |
| inclination: | 70.9756° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 356.0640° |
| argument of perigee: | 262.4289° |
| revolutions per day: | 14.14814824 |
| mean anomaly at epoch: | 108.4804° |
| orbit number at epoch: | 95301 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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