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 20453U 90008B 13145.18350636 .00007505 00000-0 51374-3 0 6860
2 20453 035.6277 230.0000 0344669 177.8960 182.3280 14.68008904228647
| Epoch (UTC): | 25 May 2013 04:24:14 |
| Eccentricity: | 0.0344669 |
| inclination: | 35.6277° |
| perigee height: | 424 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 230.0000° |
| argument of perigee: | 177.8960° |
| revolutions per day: | 14.68008904 |
| mean anomaly at epoch: | 182.3280° |
| orbit number at epoch: | 22864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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