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 26039.86619860 +.00000000 +00000-0 +23445-3 0 00001
2 31793 70.9734 232.9720 0001953 277.6316 179.0354 14.14832020 04
| Epoch (UTC): | 08 February 2026 20:47:19 |
| Eccentricity: | 0.0001953 |
| inclination: | 70.9734° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 232.9720° |
| argument of perigee: | 277.6316° |
| revolutions per day: | 14.14832020 |
| mean anomaly at epoch: | 179.0354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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