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 31117U 26076.82951986 +.00000000 +00000-0 +17504-3 0 00005
2 31117 98.0500 32.7855 0005959 49.4199 310.7530 14.79541633 03
| Epoch (UTC): | 17 March 2026 19:54:30 |
| Eccentricity: | 0.0005959 |
| inclination: | 98.0500° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 32.7855° |
| argument of perigee: | 49.4199° |
| revolutions per day: | 14.79541633 |
| mean anomaly at epoch: | 310.7530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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