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 26072.96920815 +.00000000 +00000-0 +14069-3 0 00006
2 31793 70.9758 163.3899 0002285 276.3297 257.2299 14.14835008 03
| Epoch (UTC): | 13 March 2026 23:15:39 |
| Eccentricity: | 0.0002285 |
| inclination: | 70.9758° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 163.3899° |
| argument of perigee: | 276.3297° |
| revolutions per day: | 14.14835008 |
| mean anomaly at epoch: | 257.2299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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