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 00022U 59009A 24254.76870828 .00021709 00000-0 11666-2 0 9991
2 00022 50.2781 3.0549 0107057 82.3802 278.9295 15.09949249702321
| Epoch (UTC): | 10 September 2024 18:26:56 |
| Eccentricity: | 0.0107057 |
| inclination: | 50.2781° |
| perigee height: | 462 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 3.0549° |
| argument of perigee: | 82.3802° |
| revolutions per day: | 15.09949249 |
| mean anomaly at epoch: | 278.9295° |
| orbit number at epoch: | 70232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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