View from above orbital plane
|
View from above satellite
|
Ground track
|
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,
|
|