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 22180.56812643 .00000040 00000-0 32928-4 0 9999
2 22826 98.8801 211.7400 0009109 10.4981 349.6389 14.30523754500149
| Epoch (UTC): | 29 June 2022 13:38:06 |
| Eccentricity: | 0.0009109 |
| inclination: | 98.8801° |
| perigee height: | 783 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 211.7400° |
| argument of perigee: | 10.4981° |
| revolutions per day: | 14.30523754 |
| mean anomaly at epoch: | 349.6389° |
| orbit number at epoch: | 50014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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