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 26474U 00047B 13142.05993184 .00001717 00000-0 17776-3 0 3085
2 26474 067.9977 332.5440 0061100 157.5657 202.8177 14.91267845693265
| Epoch (UTC): | 22 May 2013 01:26:18 |
| Eccentricity: | 0.0061100 |
| inclination: | 67.9977° |
| perigee height: | 551 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 332.5440° |
| argument of perigee: | 157.5657° |
| revolutions per day: | 14.91267845 |
| mean anomaly at epoch: | 202.8177° |
| orbit number at epoch: | 69326 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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