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 13139.82802169 .00029544 00000-0 47941-3 0 235
2 00063 048.5143 086.7156 0014876 078.9192 281.3425 15.52280669859372
| Epoch (UTC): | 19 May 2013 19:52:21 |
| Eccentricity: | 0.0014876 |
| inclination: | 48.5143° |
| perigee height: | 400 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 86.7156° |
| argument of perigee: | 78.9192° |
| revolutions per day: | 15.52280669 |
| mean anomaly at epoch: | 281.3425° |
| orbit number at epoch: | 85937 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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