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 18171.85653617 -.00000065 00000-0 18610-4 0 9998
2 00022 50.2846 274.5059 0140856 0.0054 0.0872 14.94567426116481
| Epoch (UTC): | 20 June 2018 20:33:24 |
| Eccentricity: | 0.0140856 |
| inclination: | 50.2846° |
| perigee height: | 485 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 274.5059° |
| argument of perigee: | 0.0054° |
| revolutions per day: | 14.94567426 |
| mean anomaly at epoch: | 0.0872° |
| orbit number at epoch: | 11648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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