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 20624U 90046A 13143.19769846 .00000096 00000-0 75262-4 0 6533
2 20624 071.0403 084.3663 0013640 139.4227 319.0131 14.13991044187126
| Epoch (UTC): | 23 May 2013 04:44:41 |
| Eccentricity: | 0.0013640 |
| inclination: | 71.0403° |
| perigee height: | 836 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 84.3663° |
| argument of perigee: | 139.4227° |
| revolutions per day: | 14.13991044 |
| mean anomaly at epoch: | 319.0131° |
| orbit number at epoch: | 18712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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