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 26134.56310573 +.00000000 +00000-0 +22154-4 0 00006
2 00117 66.8119 87.1175 0082242 317.7120 41.7635 13.90187257 09
| Epoch (UTC): | 14 May 2026 13:30:52 |
| Eccentricity: | 0.0082242 |
| inclination: | 66.8119° |
| perigee height: | 868 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 87.1175° |
| argument of perigee: | 317.7120° |
| revolutions per day: | 13.90187257 |
| mean anomaly at epoch: | 41.7635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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