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 26128.16020457 +.00000000 +00000-0 +47182-4 0 00002
2 00117 66.8107 102.7276 0081860 321.9247 37.6063 13.90186621 07
| Epoch (UTC): | 08 May 2026 03:50:41 |
| Eccentricity: | 0.0081860 |
| inclination: | 66.8107° |
| perigee height: | 868 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 102.7276° |
| argument of perigee: | 321.9247° |
| revolutions per day: | 13.90186621 |
| mean anomaly at epoch: | 37.6063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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