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 23151.71591834 .00001653 00000-0 16897-3 0 9995
2 22626 82.5195 150.1833 0020271 97.0347 263.3177 14.89828919629233
| Epoch (UTC): | 31 May 2023 17:10:55 |
| Eccentricity: | 0.0020271 |
| inclination: | 82.5195° |
| perigee height: | 584 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 150.1833° |
| argument of perigee: | 97.0347° |
| revolutions per day: | 14.89828919 |
| mean anomaly at epoch: | 263.3177° |
| orbit number at epoch: | 62923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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