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 17295U 87003A 14070.17966641 .00005609 00000-0 35985-3 0 2709
2 17295 082.5177 235.4569 0006247 276.3321 136.9795 15.08298281478512
| Epoch (UTC): | 11 March 2014 04:18:43 |
| Eccentricity: | 0.0006247 |
| inclination: | 82.5177° |
| perigee height: | 537 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 235.4569° |
| argument of perigee: | 276.3321° |
| revolutions per day: | 15.08298281 |
| mean anomaly at epoch: | 136.9795° |
| orbit number at epoch: | 47851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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