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 25348.29592179 .00000121 00000-0 90811-4 0 9993
2 31792 70.9367 22.6127 0003748 21.2640 338.8636 14.12890237952036
| Epoch (UTC): | 14 December 2025 07:06:07 |
| Eccentricity: | 0.0003748 |
| inclination: | 70.9367° |
| perigee height: | 847 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 22.6127° |
| argument of perigee: | 21.2640° |
| revolutions per day: | 14.12890237 |
| mean anomaly at epoch: | 338.8636° |
| orbit number at epoch: | 95203 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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