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 19316.13688505 .00000175 00000-0 36373-4 0 9992
2 22 50.2851 46.2835 0140114 144.7776 216.2530 14.94984918192662
| Epoch (UTC): | 12 November 2019 03:17:06 |
| Eccentricity: | 0.0140114 |
| inclination: | 50.2851° |
| perigee height: | 485 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 46.2835° |
| argument of perigee: | 144.7776° |
| revolutions per day: | 14.94984918 |
| mean anomaly at epoch: | 216.2530° |
| orbit number at epoch: | 19266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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