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 6305U 72097A 18112.75861920 -.00000037 +00000-0 +14170-4 0 9998
2 6305 099.9800 019.0310 0007968 209.3566 216.3615 13.44119295224715
| Epoch (UTC): | 22 April 2018 18:12:24 |
| Eccentricity: | 0.0007968 |
| inclination: | 99.9800° |
| perigee height: | 1088 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 19.0310° |
| argument of perigee: | 209.3566° |
| revolutions per day: | 13.44119295 |
| mean anomaly at epoch: | 216.3615° |
| orbit number at epoch: | 22471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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