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 22U 59009A 24255.76139354 .00021233 00000-0 11403-2 0 9995
2 22 50.2783 358.2882 0106981 86.2566 275.0612 15.09991012457438
| Epoch (UTC): | 11 September 2024 18:16:24 |
| Eccentricity: | 0.0106981 |
| inclination: | 50.2783° |
| perigee height: | 462 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 358.2882° |
| argument of perigee: | 86.2566° |
| revolutions per day: | 15.09991012 |
| mean anomaly at epoch: | 275.0612° |
| orbit number at epoch: | 45743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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