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 20528U 90023B 13137.52107664 .00000077 00000-0 67810-4 0 4453
2 20528 082.9355 085.3976 0031466 208.2086 270.4269 13.72714976160379
| Epoch (UTC): | 17 May 2013 12:30:21 |
| Eccentricity: | 0.0031466 |
| inclination: | 82.9355° |
| perigee height: | 966 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 85.3976° |
| argument of perigee: | 208.2086° |
| revolutions per day: | 13.72714976 |
| mean anomaly at epoch: | 270.4269° |
| orbit number at epoch: | 16037 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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