View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33498U 09002G 22175.88998423 .00000951 00000-0 13293-3 0 9992
2 33498 98.1687 68.0180 0009557 222.9800 137.0665 14.80010247722534
Epoch (UTC): | 24 June 2022 21:21:34 |
Eccentricity: | 0.0009557 |
inclination: | 98.1687° |
perigee height: | 622 km |
apogee height: | 636 km |
right ascension of ascending node: | 68.0180° |
argument of perigee: | 222.9800° |
revolutions per day: | 14.80010247 |
mean anomaly at epoch: | 137.0665° |
orbit number at epoch: | 72253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|