View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33496U 09002E 25143.69609500 .00000449 00000-0 75559-4 0 9998
2 33496 98.1710 40.8086 0005999 166.9490 193.1874 14.74433021876582
Epoch (UTC): | 23 May 2025 16:42:22 |
Eccentricity: | 0.0005999 |
inclination: | 98.1710° |
perigee height: | 643 km |
apogee height: | 651 km |
right ascension of ascending node: | 40.8086° |
argument of perigee: | 166.9490° |
revolutions per day: | 14.74433021 |
mean anomaly at epoch: | 193.1874° |
orbit number at epoch: | 87658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|