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 22006U 92036A 17206.23546983 +.00000041 +00000-0 +27147-4 0 9996
2 22006 082.9363 307.7637 0036440 338.2884 080.4594 13.74913928257651
| Epoch (UTC): | 25 July 2017 05:39:04 |
| Eccentricity: | 0.0036440 |
| inclination: | 82.9363° |
| perigee height: | 955 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 307.7637° |
| argument of perigee: | 338.2884° |
| revolutions per day: | 13.74913928 |
| mean anomaly at epoch: | 80.4594° |
| orbit number at epoch: | 25765 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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