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 32476U 08002A 13049.98778591 0.00020000 00000-0 48811-3 0 03
2 32476 40.9157 357.4533 0023256 90.9647 269.0347 15.39691276 03
| Epoch (UTC): | 18 February 2013 23:42:24 |
| Eccentricity: | 0.0023256 |
| inclination: | 40.9157° |
| perigee height: | 431 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 357.4533° |
| argument of perigee: | 90.9647° |
| revolutions per day: | 15.39691276 |
| mean anomaly at epoch: | 269.0347° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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