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 21147U 91017A 11083.88616256 0.00000250 00000-0 35917-4 0 07
2 21147 67.9850 102.4518 0005000 214.0069 145.9930 14.76331375 01
Epoch (UTC): | 24 March 2011 21:16:04 |
Eccentricity: | 0.0005000 |
inclination: | 67.9850° |
perigee height: | 637 km |
apogee height: | 644 km |
right ascension of ascending node: | 102.4518° |
argument of perigee: | 214.0069° |
revolutions per day: | 14.76331375 |
mean anomaly at epoch: | 145.9930° |
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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