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 data is extracted from the following two-line orbital elements,
1 00116U 61015A 22175.46660558 -.00000014 00000-0 48160-4 0 9997
2 00116 66.8081 206.4279 0079860 216.6865 142.8732 13.91833984 94361
| Epoch (UTC): | 24 June 2022 11:11:54 |
| Eccentricity: | 0.0079860 |
| inclination: | 66.8081° |
| perigee height: | 864 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 206.4279° |
| argument of perigee: | 216.6865° |
| revolutions per day: | 13.91833984 |
| mean anomaly at epoch: | 142.8732° |
| orbit number at epoch: | 9436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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