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 35008U 09029A 18112.00221251 -.00000049 +00000-0 +10000-3 0 9990
2 35008 064.2202 351.3038 7246674 251.6968 022.6927 02.24492014073006
Epoch (UTC): | 22 April 2018 00:03:11 |
Eccentricity: | 0.7246674 |
inclination: | 64.2202° |
perigee height: | 405 km |
apogee height: | 36113 km |
right ascension of ascending node: | 351.3038° |
argument of perigee: | 251.6968° |
revolutions per day: | 2.24492014 |
mean anomaly at epoch: | 22.6927° |
orbit number at epoch: | 7300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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