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 13168.81859023 .00000049 00000-0 33983-4 0 7071
2 20442 098.4400 110.6145 0012787 143.4885 269.5551 14.32391755222521
| Epoch (UTC): | 17 June 2013 19:38:46 |
| Eccentricity: | 0.0012787 |
| inclination: | 98.4400° |
| perigee height: | 774 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 110.6145° |
| argument of perigee: | 143.4885° |
| revolutions per day: | 14.32391755 |
| mean anomaly at epoch: | 269.5551° |
| orbit number at epoch: | 22252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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