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 22626U 93024A 23154.46961318 .00001775 00000-0 18160-3 0 9998
2 22626 82.5197 147.5783 0020294 88.6732 271.6812 14.89838867629969
| Epoch (UTC): | 03 June 2023 11:16:14 |
| Eccentricity: | 0.0020294 |
| inclination: | 82.5197° |
| perigee height: | 584 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 147.5783° |
| argument of perigee: | 88.6732° |
| revolutions per day: | 14.89838867 |
| mean anomaly at epoch: | 271.6812° |
| orbit number at epoch: | 62996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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