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 13139.45643600 -.00000085 00000-0 -12096-7 0 7571
2 27665 039.5747 133.8019 0008471 303.4414 189.7576 14.28048428537882
| Epoch (UTC): | 19 May 2013 10:57:16 |
| Eccentricity: | 0.0008471 |
| inclination: | 39.5747° |
| perigee height: | 792 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 133.8019° |
| argument of perigee: | 303.4414° |
| revolutions per day: | 14.28048428 |
| mean anomaly at epoch: | 189.7576° |
| orbit number at epoch: | 53788 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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