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 24278U 96046B 13142.17246623 .00000044 00000-0 83002-4 0 1223
2 24278 098.5574 204.2159 0349890 231.4190 140.5682 13.53000488827790
| Epoch (UTC): | 22 May 2013 04:08:21 |
| Eccentricity: | 0.0349890 |
| inclination: | 98.5574° |
| perigee height: | 801 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 204.2159° |
| argument of perigee: | 231.4190° |
| revolutions per day: | 13.53000488 |
| mean anomaly at epoch: | 140.5682° |
| orbit number at epoch: | 82779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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