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 5485U 71080A 19051.67632305 +.00000022 +00000-0 +12333-4 0 9996
2 5485 032.0538 149.8943 0640145 004.1137 356.4409 12.74133335208114
| Epoch (UTC): | 20 February 2019 16:13:54 |
| Eccentricity: | 0.0640145 |
| inclination: | 32.0538° |
| perigee height: | 869 km |
| apogee height: | 1861 km |
| right ascension of ascending node: | 149.8943° |
| argument of perigee: | 4.1137° |
| revolutions per day: | 12.74133335 |
| mean anomaly at epoch: | 356.4409° |
| orbit number at epoch: | 20811 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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