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 23405U 94077B 15064.64567243 -.00000213 00000-0 -85125-4 0 9997
2 23405 070.9838 169.9769 0002474 205.4645 154.6356 14.15144426 47442
| Epoch (UTC): | 05 March 2015 15:29:46 |
| Eccentricity: | 0.0002474 |
| inclination: | 70.9838° |
| perigee height: | 840 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 169.9769° |
| argument of perigee: | 205.4645° |
| revolutions per day: | 14.15144426 |
| mean anomaly at epoch: | 154.6356° |
| orbit number at epoch: | 4744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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