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 27665U 03005C 13143.44597361 .00000097 00000-0 72411-4 0 7606
2 27665 039.5752 113.5008 0007970 328.8454 180.4013 14.28047301538456
| Epoch (UTC): | 23 May 2013 10:42:12 |
| Eccentricity: | 0.0007970 |
| inclination: | 39.5752° |
| perigee height: | 792 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 113.5008° |
| argument of perigee: | 328.8454° |
| revolutions per day: | 14.28047301 |
| mean anomaly at epoch: | 180.4013° |
| orbit number at epoch: | 53845 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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