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 16274.57755572 -.00000101 00000-0 -11200-3 0 9994
2 00005 34.2469 84.4692 1847536 11.7521 352.0757 10.84723465 58090
| Epoch (UTC): | 30 September 2016 13:51:40 |
| Eccentricity: | 0.1847536 |
| inclination: | 34.2469° |
| perigee height: | 649 km |
| apogee height: | 3835 km |
| right ascension of ascending node: | 84.4692° |
| argument of perigee: | 11.7521° |
| revolutions per day: | 10.84723465 |
| mean anomaly at epoch: | 352.0757° |
| orbit number at epoch: | 5809 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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