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 28158U 04004A 13119.36241930 0.00000000 00000-0 00000-0 0 08
2 28158 5.1602 57.8768 0005001 35.9443 324.0965 1.00273011 09
| Epoch (UTC): | 29 April 2013 08:41:53 |
| Eccentricity: | 0.0005001 |
| inclination: | 5.1602° |
| perigee height: | 35765 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 57.8768° |
| argument of perigee: | 35.9443° |
| revolutions per day: | 1.00273011 |
| mean anomaly at epoch: | 324.0965° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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