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 is defined by the following mean orbital elements,
1 37773U 11040A 11217.69136966 +.00002254 -71274-5 +00000-0 0 9991
2 37773 028.7890 020.5966 0025801 264.4436 221.8704 16.26214442000002
| Epoch (UTC): | 05 August 2011 16:35:34 |
| Eccentricity: | 0.0025801 |
| inclination: | 28.7890° |
| perigee height: | 186 km |
| apogee height: | 220 km |
| right ascension of ascending node: | 20.5966° |
| argument of perigee: | 264.4436° |
| revolutions per day: | 16.26214442 |
| mean anomaly at epoch: | 221.8704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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