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 23605U 95033A 18111.87988871 0.00000290 00000-0 29341-4 0 01
2 23605 98.2105 177.2567 0011325 143.5994 216.4004 14.91001752 02
Epoch (UTC): | 21 April 2018 21:07:02 |
Eccentricity: | 0.0011325 |
inclination: | 98.2105° |
perigee height: | 587 km |
apogee height: | 603 km |
right ascension of ascending node: | 177.2567° |
argument of perigee: | 143.5994° |
revolutions per day: | 14.91001752 |
mean anomaly at epoch: | 216.4004° |
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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