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 22565U 93016A 24357.64077151 -.00000204 00000-0 -83821-4 0 9995
2 22565 70.8084 17.9463 0007060 330.3938 29.6781 14.12518190636887
| Epoch (UTC): | 22 December 2024 15:22:42 |
| Eccentricity: | 0.0007060 |
| inclination: | 70.8084° |
| perigee height: | 845 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 17.9463° |
| argument of perigee: | 330.3938° |
| revolutions per day: | 14.12518190 |
| mean anomaly at epoch: | 29.6781° |
| orbit number at epoch: | 63688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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