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 26140.13033029 +.00000000 +00000-0 -11914-3 0 00000
2 31793 70.9770 22.2093 0002771 267.2079 245.8333 14.14849434 03
| Epoch (UTC): | 20 May 2026 03:07:40 |
| Eccentricity: | 0.0002771 |
| inclination: | 70.9770° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 22.2093° |
| argument of perigee: | 267.2079° |
| revolutions per day: | 14.14849434 |
| mean anomaly at epoch: | 245.8333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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