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 26073.84333150 +.00000000 +00000-0 +54354-4 0 00002
2 00117 66.8109 235.1460 0077658 358.8884 1.2009 13.90180061 00
| Epoch (UTC): | 14 March 2026 20:14:23 |
| Eccentricity: | 0.0077658 |
| inclination: | 66.8109° |
| perigee height: | 871 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 235.1460° |
| argument of perigee: | 358.8884° |
| revolutions per day: | 13.90180061 |
| mean anomaly at epoch: | 1.2009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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