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 35870U 09049F 13145.76566755 .00006997 00000-0 26689-3 0 903
2 35870 097.1929 175.3141 0003508 062.0719 058.0721 15.26968039204834
| Epoch (UTC): | 25 May 2013 18:22:33 |
| Eccentricity: | 0.0003508 |
| inclination: | 97.1929° |
| perigee height: | 482 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 175.3141° |
| argument of perigee: | 62.0719° |
| revolutions per day: | 15.26968039 |
| mean anomaly at epoch: | 58.0721° |
| orbit number at epoch: | 20483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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