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 28352U 04021A 15060.47553558 .00000105 00000-0 83983-4 0 9992
2 28352 071.0032 075.5587 0017513 284.5217 227.9878 14.11400381552501
| Epoch (UTC): | 01 March 2015 11:24:46 |
| Eccentricity: | 0.0017513 |
| inclination: | 71.0032° |
| perigee height: | 842 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 75.5587° |
| argument of perigee: | 284.5217° |
| revolutions per day: | 14.11400381 |
| mean anomaly at epoch: | 227.9878° |
| orbit number at epoch: | 55250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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