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 15025.82041458 .00000183 00000-0 24786-3 0 3216
2 00005 034.2415 174.7506 1844021 130.5191 247.1250 10.84479504991446
| Epoch (UTC): | 25 January 2015 19:41:23 |
| Eccentricity: | 0.1844021 |
| inclination: | 34.2415° |
| perigee height: | 653 km |
| apogee height: | 3833 km |
| right ascension of ascending node: | 174.7506° |
| argument of perigee: | 130.5191° |
| revolutions per day: | 10.84479504 |
| mean anomaly at epoch: | 247.1250° |
| orbit number at epoch: | 99144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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