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 26137.70044779 +.00000000 +00000-0 -97461-4 0 00005
2 31793 70.9774 27.3171 0002790 267.6988 112.5147 14.14850510 04
| Epoch (UTC): | 17 May 2026 16:48:38 |
| Eccentricity: | 0.0002790 |
| inclination: | 70.9774° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 27.3171° |
| argument of perigee: | 267.6988° |
| revolutions per day: | 14.14850510 |
| mean anomaly at epoch: | 112.5147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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