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 22176.79114990 .00000060 00000-0 40930-4 0 9993
2 22826 98.8803 207.8837 0009313 21.1202 339.0362 14.30523002499858
| Epoch (UTC): | 25 June 2022 18:59:15 |
| Eccentricity: | 0.0009313 |
| inclination: | 98.8803° |
| perigee height: | 783 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 207.8837° |
| argument of perigee: | 21.1202° |
| revolutions per day: | 14.30523002 |
| mean anomaly at epoch: | 339.0362° |
| orbit number at epoch: | 49985 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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