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 15592U 85020A 13138.55828647 .00006447 00000-0 34849-3 0 1666
2 15592 082.5442 358.9524 0019654 005.2752 025.3880 15.14350437537498
| Epoch (UTC): | 18 May 2013 13:23:55 |
| Eccentricity: | 0.0019654 |
| inclination: | 82.5442° |
| perigee height: | 509 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 358.9524° |
| argument of perigee: | 5.2752° |
| revolutions per day: | 15.14350437 |
| mean anomaly at epoch: | 25.3880° |
| orbit number at epoch: | 53749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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