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 20478U 90013A 13137.83016949 .00000084 00000-0 94927-4 0 9907
2 20478 099.0940 085.6832 0005310 194.4213 219.1854 13.95147334105779
| Epoch (UTC): | 17 May 2013 19:55:26 |
| Eccentricity: | 0.0005310 |
| inclination: | 99.0940° |
| perigee height: | 907 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 85.6832° |
| argument of perigee: | 194.4213° |
| revolutions per day: | 13.95147334 |
| mean anomaly at epoch: | 219.1854° |
| orbit number at epoch: | 10577 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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