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 22146.91946394 .00005107 00000-0 38713-3 0 9995
2 00022 50.2834 15.2695 0135199 87.8527 273.7896 14.96875395576402
| Epoch (UTC): | 26 May 2022 22:04:01 |
| Eccentricity: | 0.0135199 |
| inclination: | 50.2834° |
| perigee height: | 482 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 15.2695° |
| argument of perigee: | 87.8527° |
| revolutions per day: | 14.96875395 |
| mean anomaly at epoch: | 273.7896° |
| orbit number at epoch: | 57640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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