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 19345.14603034 -.00000058 00000-0 18764-4 0 9994
2 22 50.2851 270.2051 0139894 255.5686 102.9702 14.95004754197002
| Epoch (UTC): | 11 December 2019 03:30:17 |
| Eccentricity: | 0.0139894 |
| inclination: | 50.2851° |
| perigee height: | 485 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 270.2051° |
| argument of perigee: | 255.5686° |
| revolutions per day: | 14.95004754 |
| mean anomaly at epoch: | 102.9702° |
| orbit number at epoch: | 19700 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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