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 26049.16683789 +.00000000 +00000-0 +66171-4 0 00006
2 00117 66.8127 295.3068 0075616 16.3503 343.9989 13.90176530 07
| Epoch (UTC): | 18 February 2026 04:00:14 |
| Eccentricity: | 0.0075616 |
| inclination: | 66.8127° |
| perigee height: | 873 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 295.3068° |
| argument of perigee: | 16.3503° |
| revolutions per day: | 13.90176530 |
| mean anomaly at epoch: | 343.9989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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