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 14453U 83109B 13144.18103374 .00000096 00000-0 33853-4 0 8796
2 14453 081.1651 159.9499 0105679 039.5793 027.2645 14.24391363536108
| Epoch (UTC): | 24 May 2013 04:20:41 |
| Eccentricity: | 0.0105679 |
| inclination: | 81.1651° |
| perigee height: | 734 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 159.9499° |
| argument of perigee: | 39.5793° |
| revolutions per day: | 14.24391363 |
| mean anomaly at epoch: | 27.2645° |
| orbit number at epoch: | 53610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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