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 13145.17192277 .00007215 00000-0 24529-3 0 4479
2 35867 097.1854 179.8552 0007450 203.5155 187.1104 15.30718375205109
| Epoch (UTC): | 25 May 2013 04:07:34 |
| Eccentricity: | 0.0007450 |
| inclination: | 97.1854° |
| perigee height: | 468 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 179.8552° |
| argument of perigee: | 203.5155° |
| revolutions per day: | 15.30718375 |
| mean anomaly at epoch: | 187.1104° |
| orbit number at epoch: | 20510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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