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 36800U 10035F 13138.18690521 .00002240 00000-0 24328-3 0 9499
2 36800 097.9798 225.2208 0024338 214.0153 145.9504 14.88966531154767
| Epoch (UTC): | 18 May 2013 04:29:08 |
| Eccentricity: | 0.0024338 |
| inclination: | 97.9798° |
| perigee height: | 584 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 225.2208° |
| argument of perigee: | 214.0153° |
| revolutions per day: | 14.88966531 |
| mean anomaly at epoch: | 145.9504° |
| orbit number at epoch: | 15476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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