View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24954U 97052B 25131.90274322 .00000076 00000-0 58274-4 0 9991
2 24954 82.9201 284.9686 0039340 2.8510 161.5282 13.80306561391647
Epoch (UTC): | 11 May 2025 21:39:57 |
Eccentricity: | 0.0039340 |
inclination: | 82.9201° |
perigee height: | 934 km |
apogee height: | 991 km |
right ascension of ascending node: | 284.9686° |
argument of perigee: | 2.8510° |
revolutions per day: | 13.80306561 |
mean anomaly at epoch: | 161.5282° |
orbit number at epoch: | 39164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|