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 21907U 92013B 13138.76369747 -.00000179 00000-0 00000+0 0 7466
2 21907 019.6082 025.7555 6957804 004.4137 210.7616 02.25607745174636
| Epoch (UTC): | 18 May 2013 18:19:43 |
| Eccentricity: | 0.6957804 |
| inclination: | 19.6082° |
| perigee height: | 1092 km |
| apogee height: | 35264 km |
| right ascension of ascending node: | 25.7555° |
| argument of perigee: | 4.4137° |
| revolutions per day: | 2.25607745 |
| mean anomaly at epoch: | 210.7616° |
| orbit number at epoch: | 17463 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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