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 26040.85591581 +.00000000 +00000-0 +22398-3 0 00007
2 31793 70.9736 230.8915 0001992 278.2299 177.9618 14.14832951 02
| Epoch (UTC): | 09 February 2026 20:32:31 |
| Eccentricity: | 0.0001992 |
| inclination: | 70.9736° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 230.8915° |
| argument of perigee: | 278.2299° |
| revolutions per day: | 14.14832951 |
| mean anomaly at epoch: | 177.9618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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