View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00045U 60007A 24309.57415702 .00002542 00000-0 63695-3 0 9996
2 00045 66.6934 118.8683 0257155 230.5151 127.2957 14.35077433295413
Epoch (UTC): | 04 November 2024 13:46:47 |
Eccentricity: | 0.0257155 |
inclination: | 66.6934° |
perigee height: | 591 km |
apogee height: | 959 km |
right ascension of ascending node: | 118.8683° |
argument of perigee: | 230.5151° |
revolutions per day: | 14.35077433 |
mean anomaly at epoch: | 127.2957° |
orbit number at epoch: | 29541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|