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 19884U 89021C 14105.80662159 .00023459 00000-0 16856-2 0 9427
2 19884 026.3653 171.5344 6115364 257.1654 034.1929 03.91494254287105
| Epoch (UTC): | 15 April 2014 19:21:32 |
| Eccentricity: | 0.6115364 |
| inclination: | 26.3653° |
| perigee height: | 228 km |
| apogee height: | 21026 km |
| right ascension of ascending node: | 171.5344° |
| argument of perigee: | 257.1654° |
| revolutions per day: | 3.91494254 |
| mean anomaly at epoch: | 34.1929° |
| orbit number at epoch: | 28710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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