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 44909U 19096E 22177.18159828 .00000030 00000-0 82437-4 0 9993
2 44909 82.5209 224.4770 0216307 299.4950 58.4730 12.79713614116665
| Epoch (UTC): | 26 June 2022 04:21:30 |
| Eccentricity: | 0.0216307 |
| inclination: | 82.5209° |
| perigee height: | 1175 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 224.4770° |
| argument of perigee: | 299.4950° |
| revolutions per day: | 12.79713614 |
| mean anomaly at epoch: | 58.4730° |
| orbit number at epoch: | 11666 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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