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 26158.92722367 +.00000000 +00000-0 +18580-3 0 00001
2 31793 70.9759 342.6951 0002239 258.5790 207.0203 14.14849857 09
| Epoch (UTC): | 07 June 2026 22:15:12 |
| Eccentricity: | 0.0002239 |
| inclination: | 70.9759° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 342.6951° |
| argument of perigee: | 258.5790° |
| revolutions per day: | 14.14849857 |
| mean anomaly at epoch: | 207.0203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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