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 17235.08607479 -.00000035 00000-0 21063-5 0 9997
2 27422 98.2328 231.6753 0013204 42.7701 317.4507 14.29255453796233
| Epoch (UTC): | 23 August 2017 02:03:56 |
| Eccentricity: | 0.0013204 |
| inclination: | 98.2328° |
| perigee height: | 785 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 231.6753° |
| argument of perigee: | 42.7701° |
| revolutions per day: | 14.29255453 |
| mean anomaly at epoch: | 317.4507° |
| orbit number at epoch: | 79623 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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