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 26906U 01040B 13142.94088559 0.00000090 00000-0 13398-3 0 06
2 26906 63.4726 179.0569 0223000 347.6104 12.3896 13.43860296 03
| Epoch (UTC): | 22 May 2013 22:34:52 |
| Eccentricity: | 0.0223000 |
| inclination: | 63.4726° |
| perigee height: | 928 km |
| apogee height: | 1261 km |
| right ascension of ascending node: | 179.0569° |
| argument of perigee: | 347.6104° |
| revolutions per day: | 13.43860296 |
| mean anomaly at epoch: | 12.3896° |
| 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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