View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 56276U 22151ACU 24279.76767273 .00005814 00000-0 28014-2 0 9991
2 56276 98.8000 288.7185 0008195 295.6196 64.4132 14.19056491 80304
Epoch (UTC): | 05 October 2024 18:25:26 |
Eccentricity: | 0.0008195 |
inclination: | 98.8000° |
perigee height: | 822 km |
apogee height: | 834 km |
right ascension of ascending node: | 288.7185° |
argument of perigee: | 295.6196° |
revolutions per day: | 14.19056491 |
mean anomaly at epoch: | 64.4132° |
orbit number at epoch: | 8030 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|