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 00063U 60016A 13144.84815917 .00029310 00000-0 47114-3 0 275
2 00063 048.5156 060.0692 0014677 105.2885 254.9684 15.52551280860159
| Epoch (UTC): | 24 May 2013 20:21:20 |
| Eccentricity: | 0.0014677 |
| inclination: | 48.5156° |
| perigee height: | 399 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 60.0692° |
| argument of perigee: | 105.2885° |
| revolutions per day: | 15.52551280 |
| mean anomaly at epoch: | 254.9684° |
| orbit number at epoch: | 86015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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