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 28931U 06002A 13142.24144946 .00001095 00000-0 23553-3 0 1567
2 28931 098.0329 207.9777 0001005 044.7241 315.4047 14.60399758390258
| Epoch (UTC): | 22 May 2013 05:47:41 |
| Eccentricity: | 0.0001005 |
| inclination: | 98.0329° |
| perigee height: | 691 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 207.9777° |
| argument of perigee: | 44.7241° |
| revolutions per day: | 14.60399758 |
| mean anomaly at epoch: | 315.4047° |
| orbit number at epoch: | 39025 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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