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 26040.01099402 +.00000000 +00000-0 +22908-3 0 00007
2 31793 70.9734 232.6676 0001958 277.7628 196.1853 14.14832119 06
| Epoch (UTC): | 09 February 2026 00:15:49 |
| Eccentricity: | 0.0001958 |
| inclination: | 70.9734° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 232.6676° |
| argument of perigee: | 277.7628° |
| revolutions per day: | 14.14832119 |
| mean anomaly at epoch: | 196.1853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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