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 23659U 95046C 13142.89023899 .00000391 00000-0 51355-4 0 6115
2 23659 082.5318 243.8961 0026950 056.4566 082.3589 14.77476621955011
| Epoch (UTC): | 22 May 2013 21:21:56 |
| Eccentricity: | 0.0026950 |
| inclination: | 82.5318° |
| perigee height: | 618 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 243.8961° |
| argument of perigee: | 56.4566° |
| revolutions per day: | 14.77476621 |
| mean anomaly at epoch: | 82.3589° |
| orbit number at epoch: | 95501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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