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 10974U 78067B 13139.48416167 .00000443 00000-0 47682-4 0 9782
2 10974 082.4809 139.1944 0016688 232.7096 273.7019 14.86201711886218
| Epoch (UTC): | 19 May 2013 11:37:11 |
| Eccentricity: | 0.0016688 |
| inclination: | 82.4809° |
| perigee height: | 598 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 139.1944° |
| argument of perigee: | 232.7096° |
| revolutions per day: | 14.86201711 |
| mean anomaly at epoch: | 273.7019° |
| orbit number at epoch: | 88621 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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