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 20466U 90010B 13138.10248166 .00000505 00000-0 62889-4 0 6312
2 20466 082.5022 327.0437 0021087 189.6165 306.4960 14.80424317256813
| Epoch (UTC): | 18 May 2013 02:27:34 |
| Eccentricity: | 0.0021087 |
| inclination: | 82.5022° |
| perigee height: | 613 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 327.0437° |
| argument of perigee: | 189.6165° |
| revolutions per day: | 14.80424317 |
| mean anomaly at epoch: | 306.4960° |
| orbit number at epoch: | 25681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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