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 42770U 17036F 17245.93730135 +.99999999 +00000-0 +73960-1 0 9995
2 42770 097.4262 306.2162 0014869 278.7167 080.9844 16.07641391010932
Epoch (UTC): | 02 September 2017 22:29:42 |
Eccentricity: | 0.0014869 |
inclination: | 97.4262° |
perigee height: | 243 km |
apogee height: | 263 km |
right ascension of ascending node: | 306.2162° |
argument of perigee: | 278.7167° |
revolutions per day: | 16.07641391 |
mean anomaly at epoch: | 80.9844° |
orbit number at epoch: | 1093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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