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 13138.19105194 .00000557 00000-0 60610-4 0 9775
2 10974 082.4808 140.4172 0016593 237.2160 194.9265 14.86199382886028
| Epoch (UTC): | 18 May 2013 04:35:06 |
| Eccentricity: | 0.0016593 |
| inclination: | 82.4808° |
| perigee height: | 598 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 140.4172° |
| argument of perigee: | 237.2160° |
| revolutions per day: | 14.86199382 |
| mean anomaly at epoch: | 194.9265° |
| orbit number at epoch: | 88602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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