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 28647U 05016B 13166.91837440 0.00001400 00000-0 95519-4 0 03
2 28647 57.0046 166.6280 0144014 222.8552 137.1447 14.97645504 02
| Epoch (UTC): | 15 June 2013 22:02:27 |
| Eccentricity: | 0.0144014 |
| inclination: | 57.0046° |
| perigee height: | 474 km |
| apogee height: | 674 km |
| right ascension of ascending node: | 166.6280° |
| argument of perigee: | 222.8552° |
| revolutions per day: | 14.97645504 |
| mean anomaly at epoch: | 137.1447° |
| 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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