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 28649U 05017A 13169.36515712 .00000544 00000-0 72591-4 0 1467
2 28649 097.8708 244.3323 0002718 077.9121 282.2397 14.83454273439556
| Epoch (UTC): | 18 June 2013 08:45:49 |
| Eccentricity: | 0.0002718 |
| inclination: | 97.8708° |
| perigee height: | 616 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 244.3323° |
| argument of perigee: | 77.9121° |
| revolutions per day: | 14.83454273 |
| mean anomaly at epoch: | 282.2397° |
| orbit number at epoch: | 43955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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