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 26044.92218589 +.00000000 +00000-0 +57380-4 0 00009
2 00117 66.8135 305.6542 0075261 19.3925 340.9989 13.90175821 04
| Epoch (UTC): | 13 February 2026 22:07:56 |
| Eccentricity: | 0.0075261 |
| inclination: | 66.8135° |
| perigee height: | 873 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 305.6542° |
| argument of perigee: | 19.3925° |
| revolutions per day: | 13.90175821 |
| mean anomaly at epoch: | 340.9989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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