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 18109.63652332 +.00000025 +00000-0 +10504-4 0 9990
2 22006 082.9308 108.7446 0035918 309.3113 187.9967 13.74924002294530
Epoch (UTC): | 19 April 2018 15:16:35 |
Eccentricity: | 0.0035918 |
inclination: | 82.9308° |
perigee height: | 955 km |
apogee height: | 1008 km |
right ascension of ascending node: | 108.7446° |
argument of perigee: | 309.3113° |
revolutions per day: | 13.74924002 |
mean anomaly at epoch: | 187.9967° |
orbit number at epoch: | 29453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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