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 11671U 80005A 14107.85542126 .00131933 00000-0 84485-3 0 4093
2 11671 082.4694 023.4644 0005581 130.0206 271.8506 15.75879996878643
| Epoch (UTC): | 17 April 2014 20:31:48 |
| Eccentricity: | 0.0005581 |
| inclination: | 82.4694° |
| perigee height: | 338 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 23.4644° |
| argument of perigee: | 130.0206° |
| revolutions per day: | 15.75879996 |
| mean anomaly at epoch: | 271.8506° |
| orbit number at epoch: | 87864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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