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 22627U 93024B 24282.70351357 .00001823 00000-0 24084-3 0 9991
2 22627 82.5208 139.2226 0021649 234.0750 125.8454 14.79367838696695
| Epoch (UTC): | 08 October 2024 16:53:03 |
| Eccentricity: | 0.0021649 |
| inclination: | 82.5208° |
| perigee height: | 616 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 139.2226° |
| argument of perigee: | 234.0750° |
| revolutions per day: | 14.79367838 |
| mean anomaly at epoch: | 125.8454° |
| orbit number at epoch: | 69669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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