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 31793U 26106.69319720 +.00000000 +00000-0 -20422-4 0 00003
2 31793 70.9730 92.4966 0002698 271.4805 261.7754 14.14841304 01
| Epoch (UTC): | 16 April 2026 16:38:12 |
| Eccentricity: | 0.0002698 |
| inclination: | 70.9730° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 92.4966° |
| argument of perigee: | 271.4805° |
| revolutions per day: | 14.14841304 |
| mean anomaly at epoch: | 261.7754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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