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 24262.45984520 .00000017 00000-0 22768-4 0 9991
2 44909 82.5222 42.7789 0217368 192.8785 166.6712 12.79734003220901
| Epoch (UTC): | 18 September 2024 11:02:10 |
| Eccentricity: | 0.0217368 |
| inclination: | 82.5222° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 42.7789° |
| argument of perigee: | 192.8785° |
| revolutions per day: | 12.79734003 |
| mean anomaly at epoch: | 166.6712° |
| orbit number at epoch: | 22090 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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