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 26041.91815414 +.00000000 +00000-0 +20435-3 0 00009
2 31793 70.9738 228.6585 0002031 279.3733 185.6151 14.14833800 04
| Epoch (UTC): | 10 February 2026 22:02:08 |
| Eccentricity: | 0.0002031 |
| inclination: | 70.9738° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 228.6585° |
| argument of perigee: | 279.3733° |
| revolutions per day: | 14.14833800 |
| mean anomaly at epoch: | 185.6151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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