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 14207.61193491 -.00000137 00000-0 -15202-3 0 2447
2 00005 034.2480 018.6770 1849013 026.6443 341.8257 10.84386434971556
| Epoch (UTC): | 26 July 2014 14:41:11 |
| Eccentricity: | 0.1849013 |
| inclination: | 34.2480° |
| perigee height: | 650 km |
| apogee height: | 3838 km |
| right ascension of ascending node: | 18.6770° |
| argument of perigee: | 26.6443° |
| revolutions per day: | 10.84386434 |
| mean anomaly at epoch: | 341.8257° |
| orbit number at epoch: | 97155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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