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 27422U 02021B 18110.90896951 -.00000030 +00000-0 +42177-5 0 9990
2 27422 098.2533 099.4856 0013270 048.6346 311.5976 14.29260488832520
| Epoch (UTC): | 20 April 2018 21:48:54 |
| Eccentricity: | 0.0013270 |
| inclination: | 98.2533° |
| perigee height: | 784 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 99.4856° |
| argument of perigee: | 48.6346° |
| revolutions per day: | 14.29260488 |
| mean anomaly at epoch: | 311.5976° |
| orbit number at epoch: | 83252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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