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 22019.16600838 .00001553 00000-0 13550-3 0 9994
2 22 50.2836 255.8301 0137154 318.7113 40.3527 14.96075484312239
| Epoch (UTC): | 19 January 2022 03:59:03 |
| Eccentricity: | 0.0137154 |
| inclination: | 50.2836° |
| perigee height: | 483 km |
| apogee height: | 674 km |
| right ascension of ascending node: | 255.8301° |
| argument of perigee: | 318.7113° |
| revolutions per day: | 14.96075484 |
| mean anomaly at epoch: | 40.3527° |
| orbit number at epoch: | 31223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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