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 20442U 90005G 13143.87696731 .00000160 00000-0 74996-4 0 6875
2 20442 098.4389 086.3335 0011314 215.7288 177.2576 14.32384445218954
| Epoch (UTC): | 23 May 2013 21:02:49 |
| Eccentricity: | 0.0011314 |
| inclination: | 98.4389° |
| perigee height: | 775 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 86.3335° |
| argument of perigee: | 215.7288° |
| revolutions per day: | 14.32384445 |
| mean anomaly at epoch: | 177.2576° |
| orbit number at epoch: | 21895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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