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 24276.68367491 .00001650 00000-0 21779-3 0 9993
2 22627 82.5218 144.8242 0021391 255.0530 104.8315 14.79348496695814
| Epoch (UTC): | 02 October 2024 16:24:29 |
| Eccentricity: | 0.0021391 |
| inclination: | 82.5218° |
| perigee height: | 616 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 144.8242° |
| argument of perigee: | 255.0530° |
| revolutions per day: | 14.79348496 |
| mean anomaly at epoch: | 104.8315° |
| orbit number at epoch: | 69581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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