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 26134.37914675 +.00000000 +00000-0 +89030-4 0 00008
2 31117 98.0578 90.4651 0004140 195.8451 164.2632 14.79682265 03
| Epoch (UTC): | 14 May 2026 09:05:58 |
| Eccentricity: | 0.0004140 |
| inclination: | 98.0578° |
| perigee height: | 627 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 90.4651° |
| argument of perigee: | 195.8451° |
| revolutions per day: | 14.79682265 |
| mean anomaly at epoch: | 164.2632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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