View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 23342U 94074A 25193.35369398 .00000664 00000-0 85084-4 0 9999
2 23342 97.6892 219.3198 0002153 99.0339 261.1119 14.84388411653506
Epoch (UTC): | 12 July 2025 08:29:19 |
Eccentricity: | 0.0002153 |
inclination: | 97.6892° |
perigee height: | 614 km |
apogee height: | 617 km |
right ascension of ascending node: | 219.3198° |
argument of perigee: | 99.0339° |
revolutions per day: | 14.84388411 |
mean anomaly at epoch: | 261.1119° |
orbit number at epoch: | 65350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|