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 20465U 90010A 13168.24627494 .00000557 00000-0 50521-4 0 8122
2 20465 082.4917 208.8940 0018188 159.0162 201.1808 14.93369411266927
| Epoch (UTC): | 17 June 2013 05:54:38 |
| Eccentricity: | 0.0018188 |
| inclination: | 82.4917° |
| perigee height: | 575 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 208.8940° |
| argument of perigee: | 159.0162° |
| revolutions per day: | 14.93369411 |
| mean anomaly at epoch: | 201.1808° |
| orbit number at epoch: | 26692 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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