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 26017.18397627 +.00000000 +00000-0 -11647-3 0 00008
2 31793 70.9756 280.6532 0002172 273.8216 248.3034 14.14823110 05
| Epoch (UTC): | 17 January 2026 04:24:55 |
| Eccentricity: | 0.0002172 |
| inclination: | 70.9756° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 280.6532° |
| argument of perigee: | 273.8216° |
| revolutions per day: | 14.14823110 |
| mean anomaly at epoch: | 248.3034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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