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 20510U 90018A 13144.14001333 .00002080 00000-0 19131-3 0 3930
2 20510 082.5163 153.3524 0011716 308.7101 117.3733 14.94276667259254
| Epoch (UTC): | 24 May 2013 03:21:37 |
| Eccentricity: | 0.0011716 |
| inclination: | 82.5163° |
| perigee height: | 576 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 153.3524° |
| argument of perigee: | 308.7101° |
| revolutions per day: | 14.94276667 |
| mean anomaly at epoch: | 117.3733° |
| orbit number at epoch: | 25925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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