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 13142.83393564 .00000125 00000-0 61898-4 0 6865
2 20442 098.4388 085.3179 0011254 219.2644 198.3315 14.32384023218807
| Epoch (UTC): | 22 May 2013 20:00:52 |
| Eccentricity: | 0.0011254 |
| inclination: | 98.4388° |
| perigee height: | 776 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 85.3179° |
| argument of perigee: | 219.2644° |
| revolutions per day: | 14.32384023 |
| mean anomaly at epoch: | 198.3315° |
| orbit number at epoch: | 21880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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