View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 19650U 88102B 25194.02485376 .00000218 00000-0 13453-3 0 9996
2 19650 71.0007 295.7545 0013877 6.9267 353.2046 14.16109468893240
Epoch (UTC): | 13 July 2025 00:35:47 |
Eccentricity: | 0.0013877 |
inclination: | 71.0007° |
perigee height: | 828 km |
apogee height: | 848 km |
right ascension of ascending node: | 295.7545° |
argument of perigee: | 6.9267° |
revolutions per day: | 14.16109468 |
mean anomaly at epoch: | 353.2046° |
orbit number at epoch: | 89324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|