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 22148.78868695 .00004577 00000-0 34919-3 0 9993
2 22 50.2832 6.4752 0135149 95.0158 266.6233 14.96894048331649
| Epoch (UTC): | 28 May 2022 18:55:42 |
| Eccentricity: | 0.0135149 |
| inclination: | 50.2832° |
| perigee height: | 482 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 6.4752° |
| argument of perigee: | 95.0158° |
| revolutions per day: | 14.96894048 |
| mean anomaly at epoch: | 266.6233° |
| orbit number at epoch: | 33164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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