View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 04256U 69082B 22225.91376848 .00000079 00000-0 92282-4 0 9994
2 04256 70.0096 97.7199 0016974 102.9728 257.3276 13.98470190694226
Epoch (UTC): | 13 August 2022 21:55:49 |
Eccentricity: | 0.0016974 |
inclination: | 70.0096° |
perigee height: | 887 km |
apogee height: | 911 km |
right ascension of ascending node: | 97.7199° |
argument of perigee: | 102.9728° |
revolutions per day: | 13.98470190 |
mean anomaly at epoch: | 257.3276° |
orbit number at epoch: | 69422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|