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 36122U 09072B 13169.19001324 -.00000044 00000-0 00000+0 0 6504
2 36122 100.3052 226.2172 0007527 355.0643 005.0396 13.16305129168544
| Epoch (UTC): | 18 June 2013 04:33:37 |
| Eccentricity: | 0.0007527 |
| inclination: | 100.3052° |
| perigee height: | 1193 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 226.2172° |
| argument of perigee: | 355.0643° |
| revolutions per day: | 13.16305129 |
| mean anomaly at epoch: | 5.0396° |
| orbit number at epoch: | 16854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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