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 35870U 09049F 13145.10395606 .00007163 00000-0 27322-3 0 884
2 35870 097.1928 174.6761 0003530 063.7040 021.3196 15.26959636204734
| Epoch (UTC): | 25 May 2013 02:29:41 |
| Eccentricity: | 0.0003530 |
| inclination: | 97.1928° |
| perigee height: | 482 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 174.6761° |
| argument of perigee: | 63.7040° |
| revolutions per day: | 15.26959636 |
| mean anomaly at epoch: | 21.3196° |
| orbit number at epoch: | 20473 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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