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 17295.76395788 -.00000023 +00000-0 +37549-4 0 9994
2 6305 099.9861 198.5503 0007874 299.1145 129.1619 13.44115965200264
| Epoch (UTC): | 22 October 2017 18:20:05 |
| Eccentricity: | 0.0007874 |
| inclination: | 99.9861° |
| perigee height: | 1088 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 198.5503° |
| argument of perigee: | 299.1145° |
| revolutions per day: | 13.44115965 |
| mean anomaly at epoch: | 129.1619° |
| orbit number at epoch: | 20026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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