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 22826U 93061D 22182.87627779 .00000019 00000-0 25048-4 0 9990
2 22826 98.8799 214.0965 0008961 3.8090 356.3158 14.30524098500476
| Epoch (UTC): | 01 July 2022 21:01:50 |
| Eccentricity: | 0.0008961 |
| inclination: | 98.8799° |
| perigee height: | 783 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 214.0965° |
| argument of perigee: | 3.8090° |
| revolutions per day: | 14.30524098 |
| mean anomaly at epoch: | 356.3158° |
| orbit number at epoch: | 50047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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