View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25397U 98043D 24338.20835891 .00000354 00000-0 17356-3 0 9993
2 25397 98.9468 307.6675 0002095 56.2024 303.9353 14.24203460371699
Epoch (UTC): | 03 December 2024 05:00:02 |
Eccentricity: | 0.0002095 |
inclination: | 98.9468° |
perigee height: | 809 km |
apogee height: | 812 km |
right ascension of ascending node: | 307.6675° |
argument of perigee: | 56.2024° |
revolutions per day: | 14.24203460 |
mean anomaly at epoch: | 303.9353° |
orbit number at epoch: | 37169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|