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 26934U 01044A 14270.56049042 0.00016000 00000-0 20177-3 0 07
2 26934 96.9959 41.0452 0003500 14.9902 345.0096 15.59586592 04
| Epoch (UTC): | 27 September 2014 13:27:06 |
| Eccentricity: | 0.0003500 |
| inclination: | 96.9959° |
| perigee height: | 386 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 41.0452° |
| argument of perigee: | 14.9902° |
| revolutions per day: | 15.59586592 |
| mean anomaly at epoch: | 345.0096° |
| 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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