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 28941U 06005C 09297.68475575 .14491492 29743-5 25760-3 0 9996
2 28941 098.0955 138.9518 0011688 319.8691 040.7485 16.46998778207909
| Epoch (UTC): | 24 October 2009 16:26:02 |
| Eccentricity: | 0.0011688 |
| inclination: | 98.0955° |
| perigee height: | 139 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 138.9518° |
| argument of perigee: | 319.8691° |
| revolutions per day: | 16.46998778 |
| mean anomaly at epoch: | 40.7485° |
| orbit number at epoch: | 20790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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