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 15495U 85009B 14069.84515204 .00000620 00000-0 73015-4 0 7159
2 15495 082.5244 225.7732 0019040 310.7178 163.8759 14.83120010572890
| Epoch (UTC): | 10 March 2014 20:17:01 |
| Eccentricity: | 0.0019040 |
| inclination: | 82.5244° |
| perigee height: | 606 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 225.7732° |
| argument of perigee: | 310.7178° |
| revolutions per day: | 14.83120010 |
| mean anomaly at epoch: | 163.8759° |
| orbit number at epoch: | 57289 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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