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 31708U 07027C 25360.20098909 0.00000000 00000-0 00000-0 0 01
2 31708 63.3825 49.2287 0443904 22.9460 337.0540 13.40986015 06
| Epoch (UTC): | 26 December 2025 04:49:25 |
| Eccentricity: | 0.0443904 |
| inclination: | 63.3825° |
| perigee height: | 773 km |
| apogee height: | 1438 km |
| right ascension of ascending node: | 49.2287° |
| argument of perigee: | 22.9460° |
| revolutions per day: | 13.40986015 |
| mean anomaly at epoch: | 337.0540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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