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 36105U 09066B 13142.87953557 0.00004000 00000-0 28945-3 0 04
2 36105 97.5261 201.2796 0037584 46.3084 313.6914 15.03487312 07
| Epoch (UTC): | 22 May 2013 21:06:31 |
| Eccentricity: | 0.0037584 |
| inclination: | 97.5261° |
| perigee height: | 530 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 201.2796° |
| argument of perigee: | 46.3084° |
| revolutions per day: | 15.03487312 |
| mean anomaly at epoch: | 313.6914° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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