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 26037.95935683 +.00000000 +00000-0 +25832-3 0 00005
2 31793 70.9731 236.9806 0001894 276.4183 190.8427 14.14830269 08
| Epoch (UTC): | 06 February 2026 23:01:28 |
| Eccentricity: | 0.0001894 |
| inclination: | 70.9731° |
| perigee height: | 842 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 236.9806° |
| argument of perigee: | 276.4183° |
| revolutions per day: | 14.14830269 |
| mean anomaly at epoch: | 190.8427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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