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 00117U 26133.34007987 +.00000000 +00000-0 +33087-4 0 00000
2 00117 66.8116 90.0991 0082175 318.5101 40.9757 13.90187133 07
| Epoch (UTC): | 13 May 2026 08:09:42 |
| Eccentricity: | 0.0082175 |
| inclination: | 66.8116° |
| perigee height: | 868 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 90.0991° |
| argument of perigee: | 318.5101° |
| revolutions per day: | 13.90187133 |
| mean anomaly at epoch: | 40.9757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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