View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00053U 60009E 24311.81478130 -.00000046 00000-0 38460-3 0 9991
2 00053 47.2791 354.1458 0098573 140.8939 219.9026 12.17354892863879
Epoch (UTC): | 06 November 2024 19:33:17 |
Eccentricity: | 0.0098573 |
inclination: | 47.2791° |
perigee height: | 1525 km |
apogee height: | 1683 km |
right ascension of ascending node: | 354.1458° |
argument of perigee: | 140.8939° |
revolutions per day: | 12.17354892 |
mean anomaly at epoch: | 219.9026° |
orbit number at epoch: | 86387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|