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 26140.96600553 +.00000000 +00000-0 +34267-4 0 00005
2 00117 66.8128 71.5076 0082596 313.4867 45.9364 13.90187712 00
| Epoch (UTC): | 20 May 2026 23:11:02 |
| Eccentricity: | 0.0082596 |
| inclination: | 66.8128° |
| perigee height: | 868 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 71.5076° |
| argument of perigee: | 313.4867° |
| revolutions per day: | 13.90187712 |
| mean anomaly at epoch: | 45.9364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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