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 18959U 88020B 13140.34599953 .00000334 00000-0 38610-4 0 9381
2 18959 082.5393 221.2745 0016836 010.4565 057.5746 14.82483884359924
| Epoch (UTC): | 20 May 2013 08:18:14 |
| Eccentricity: | 0.0016836 |
| inclination: | 82.5393° |
| perigee height: | 610 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 221.2745° |
| argument of perigee: | 10.4565° |
| revolutions per day: | 14.82483884 |
| mean anomaly at epoch: | 57.5746° |
| orbit number at epoch: | 35992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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