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 00005U 58002B 14064.47404816 .00000007 00000-0 30456-4 0 1990
2 00005 034.2450 099.3413 1849482 103.0309 278.2246 10.84390409956038
| Epoch (UTC): | 05 March 2014 11:22:37 |
| Eccentricity: | 0.1849482 |
| inclination: | 34.2450° |
| perigee height: | 649 km |
| apogee height: | 3838 km |
| right ascension of ascending node: | 99.3413° |
| argument of perigee: | 103.0309° |
| revolutions per day: | 10.84390409 |
| mean anomaly at epoch: | 278.2246° |
| orbit number at epoch: | 95603 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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