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 28886U 05041C 13170.07729590 -.00000104 00000-0 00000+0 0 4049
2 28886 007.5149 195.8754 7198362 094.2077 343.2436 02.24287866 62978
| Epoch (UTC): | 19 June 2013 01:51:18 |
| Eccentricity: | 0.7198362 |
| inclination: | 7.5149° |
| perigee height: | 528 km |
| apogee height: | 36020 km |
| right ascension of ascending node: | 195.8754° |
| argument of perigee: | 94.2077° |
| revolutions per day: | 2.24287866 |
| mean anomaly at epoch: | 343.2436° |
| orbit number at epoch: | 6297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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