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 27424U 02022A 13139.85765550 .00000711 00000-0 16783-3 0 6694
2 27424 098.1984 081.6779 0001512 078.9626 314.6535 14.57101893587393
| Epoch (UTC): | 19 May 2013 20:35:01 |
| Eccentricity: | 0.0001512 |
| inclination: | 98.1984° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 81.6779° |
| argument of perigee: | 78.9626° |
| revolutions per day: | 14.57101893 |
| mean anomaly at epoch: | 314.6535° |
| orbit number at epoch: | 58739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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