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 24907U 97043E 13138.47686391 .00000190 00000-0 60805-4 0 3431
2 24907 086.3979 159.0532 0002333 107.5908 042.5724 14.34216712824168
| Epoch (UTC): | 18 May 2013 11:26:41 |
| Eccentricity: | 0.0002333 |
| inclination: | 86.3979° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 159.0532° |
| argument of perigee: | 107.5908° |
| revolutions per day: | 14.34216712 |
| mean anomaly at epoch: | 42.5724° |
| orbit number at epoch: | 82416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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