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 26083.77146729 +.00000000 +00000-0 +51349-4 0 00000
2 00117 66.8123 210.9423 0078482 351.9743 8.0074 13.90181082 01
| Epoch (UTC): | 24 March 2026 18:30:54 |
| Eccentricity: | 0.0078482 |
| inclination: | 66.8123° |
| perigee height: | 871 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 210.9423° |
| argument of perigee: | 351.9743° |
| revolutions per day: | 13.90181082 |
| mean anomaly at epoch: | 8.0074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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