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 19346.41602350 -.00000032 00000-0 20651-4 0 9995
2 22 50.2850 264.2478 0139876 260.4236 98.0882 14.95005576197190
| Epoch (UTC): | 12 December 2019 09:59:04 |
| Eccentricity: | 0.0139876 |
| inclination: | 50.2850° |
| perigee height: | 485 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 264.2478° |
| argument of perigee: | 260.4236° |
| revolutions per day: | 14.95005576 |
| mean anomaly at epoch: | 98.0882° |
| orbit number at epoch: | 19719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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