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 05918U 72022B 13141.79948043 .00000040 00000-0 16539-4 0 8957
2 05918 081.2361 324.5795 0058945 184.5585 255.8345 14.05643940109028
| Epoch (UTC): | 21 May 2013 19:11:15 |
| Eccentricity: | 0.0058945 |
| inclination: | 81.2361° |
| perigee height: | 831 km |
| apogee height: | 917 km |
| right ascension of ascending node: | 324.5795° |
| argument of perigee: | 184.5585° |
| revolutions per day: | 14.05643940 |
| mean anomaly at epoch: | 255.8345° |
| orbit number at epoch: | 10902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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