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 26048.73517850 +.00000000 +00000-0 +67589-4 0 00007
2 00117 66.8128 296.3590 0075581 16.6673 343.6863 13.90176482 05
| Epoch (UTC): | 17 February 2026 17:38:39 |
| Eccentricity: | 0.0075581 |
| inclination: | 66.8128° |
| perigee height: | 873 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 296.3590° |
| argument of perigee: | 16.6673° |
| revolutions per day: | 13.90176482 |
| mean anomaly at epoch: | 343.6863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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