View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 42732U 98067MM 19035.84948260 .08466551 12392-4 69401-3 0 9996
2 42732 51.6102 222.7661 0006965 282.1368 217.9093 16.38912453 97286
Epoch (UTC): | 04 February 2019 20:23:15 |
Eccentricity: | 0.0006965 |
inclination: | 51.6102° |
perigee height: | 164 km |
apogee height: | 173 km |
right ascension of ascending node: | 222.7661° |
argument of perigee: | 282.1368° |
revolutions per day: | 16.38912453 |
mean anomaly at epoch: | 217.9093° |
orbit number at epoch: | 9728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|