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 00029U 60002B 13145.46577692 .00000281 00000-0 75193-4 0 9270
2 00029 048.3787 235.3821 0024453 001.0888 359.0073 14.72635605838080
| Epoch (UTC): | 25 May 2013 11:10:43 |
| Eccentricity: | 0.0024453 |
| inclination: | 48.3787° |
| perigee height: | 635 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 235.3821° |
| argument of perigee: | 1.0888° |
| revolutions per day: | 14.72635605 |
| mean anomaly at epoch: | 359.0073° |
| orbit number at epoch: | 83808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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