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 35867U 09049C 13142.16671244 .00008177 00000-0 27801-3 0 4396
2 35867 097.1864 176.9442 0007366 215.4403 185.6922 15.30677980204645
| Epoch (UTC): | 22 May 2013 04:00:03 |
| Eccentricity: | 0.0007366 |
| inclination: | 97.1864° |
| perigee height: | 469 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 176.9442° |
| argument of perigee: | 215.4403° |
| revolutions per day: | 15.30677980 |
| mean anomaly at epoch: | 185.6922° |
| orbit number at epoch: | 20464 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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