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 13137.76820178 .00027424 00000-0 44784-3 0 211
2 00063 048.5142 097.6468 0014993 067.9854 292.2683 15.52142949859051
| Epoch (UTC): | 17 May 2013 18:26:12 |
| Eccentricity: | 0.0014993 |
| inclination: | 48.5142° |
| perigee height: | 400 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 97.6468° |
| argument of perigee: | 67.9854° |
| revolutions per day: | 15.52142949 |
| mean anomaly at epoch: | 292.2683° |
| orbit number at epoch: | 85905 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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