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 28375U 04025K 13138.94652328 .00000269 00000-0 92605-4 0 5608
2 28375 098.1988 095.5835 0084813 104.5675 297.0215 14.41111836467123
| Epoch (UTC): | 18 May 2013 22:42:59 |
| Eccentricity: | 0.0084813 |
| inclination: | 98.1988° |
| perigee height: | 694 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 95.5835° |
| argument of perigee: | 104.5675° |
| revolutions per day: | 14.41111836 |
| mean anomaly at epoch: | 297.0215° |
| orbit number at epoch: | 46712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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