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 26041.18113462 +.00000000 +00000-0 +61176-4 0 00006
2 00117 66.8141 314.7737 0074953 22.0726 338.3551 13.90175267 05
| Epoch (UTC): | 10 February 2026 04:20:50 |
| Eccentricity: | 0.0074953 |
| inclination: | 66.8141° |
| perigee height: | 873 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 314.7737° |
| argument of perigee: | 22.0726° |
| revolutions per day: | 13.90175267 |
| mean anomaly at epoch: | 338.3551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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