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 22179.51896647 .00000047 00000-0 35732-4 0 9991
2 22826 98.8801 210.6688 0009160 13.4433 346.6991 14.30523578499997
| Epoch (UTC): | 28 June 2022 12:27:18 |
| Eccentricity: | 0.0009160 |
| inclination: | 98.8801° |
| perigee height: | 783 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 210.6688° |
| argument of perigee: | 13.4433° |
| revolutions per day: | 14.30523578 |
| mean anomaly at epoch: | 346.6991° |
| orbit number at epoch: | 49999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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