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 06155U 72065B 13139.38554191 .00000798 00000-0 13536-3 0 389
2 06155 035.0040 115.5222 0040486 230.2685 129.4441 14.69220220172538
| Epoch (UTC): | 19 May 2013 09:15:10 |
| Eccentricity: | 0.0040486 |
| inclination: | 35.0040° |
| perigee height: | 635 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 115.5222° |
| argument of perigee: | 230.2685° |
| revolutions per day: | 14.69220220 |
| mean anomaly at epoch: | 129.4441° |
| orbit number at epoch: | 17253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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