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 13168.84460710 .00016851 00000-0 26505-3 0 477
2 00063 048.5150 292.5695 0015191 225.0839 134.8875 15.53506835863888
| Epoch (UTC): | 17 June 2013 20:16:14 |
| Eccentricity: | 0.0015191 |
| inclination: | 48.5150° |
| perigee height: | 396 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 292.5695° |
| argument of perigee: | 225.0839° |
| revolutions per day: | 15.53506835 |
| mean anomaly at epoch: | 134.8875° |
| orbit number at epoch: | 86388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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