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 20480U 90013C 15023.81978153 -.00000045 00000-0 -24943-4 0 9582
2 20480 099.0734 310.7465 0539934 214.1434 214.4529 12.83401489169436
| Epoch (UTC): | 23 January 2015 19:40:29 |
| Eccentricity: | 0.0539934 |
| inclination: | 99.0734° |
| perigee height: | 912 km |
| apogee height: | 1744 km |
| right ascension of ascending node: | 310.7465° |
| argument of perigee: | 214.1434° |
| revolutions per day: | 12.83401489 |
| mean anomaly at epoch: | 214.4529° |
| orbit number at epoch: | 16943 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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