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 23937U 96029F 06195.10715782 0.00000300 00000-0 21157-3 0 07
2 23937 63.3975 71.9486 0341997 4.3835 355.6165 13.73294158 04
Epoch (UTC): | 14 July 2006 02:34:18 |
Eccentricity: | 0.0341997 |
inclination: | 63.3975° |
perigee height: | 736 km |
apogee height: | 1239 km |
right ascension of ascending node: | 71.9486° |
argument of perigee: | 4.3835° |
revolutions per day: | 13.73294158 |
mean anomaly at epoch: | 355.6165° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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