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 13143.63190689 .00000358 00000-0 42456-3 0 917
2 00005 034.2602 259.2589 1850968 257.7082 081.1181 10.84302201925009
| Epoch (UTC): | 23 May 2013 15:09:56 |
| Eccentricity: | 0.1850968 |
| inclination: | 34.2602° |
| perigee height: | 648 km |
| apogee height: | 3840 km |
| right ascension of ascending node: | 259.2589° |
| argument of perigee: | 257.7082° |
| revolutions per day: | 10.84302201 |
| mean anomaly at epoch: | 81.1181° |
| orbit number at epoch: | 92500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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