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 13137.86642308 .00000450 00000-0 10134-3 0 9228
2 00029 048.3800 271.1468 0024765 328.7789 031.1650 14.72624995836960
| Epoch (UTC): | 17 May 2013 20:47:38 |
| Eccentricity: | 0.0024765 |
| inclination: | 48.3800° |
| perigee height: | 635 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 271.1468° |
| argument of perigee: | 328.7789° |
| revolutions per day: | 14.72624995 |
| mean anomaly at epoch: | 31.1650° |
| orbit number at epoch: | 83696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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