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 14781U 84021B 15031.13369640 .00000867 00000-0 11547-3 0 7291
2 14781 097.8206 091.4784 0009612 151.9471 208.2262 14.82120368661723
| Epoch (UTC): | 31 January 2015 03:12:31 |
| Eccentricity: | 0.0009612 |
| inclination: | 97.8206° |
| perigee height: | 616 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 91.4784° |
| argument of perigee: | 151.9471° |
| revolutions per day: | 14.82120368 |
| mean anomaly at epoch: | 208.2262° |
| orbit number at epoch: | 66172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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