View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25544U 98067A 23037.69601222 .00011883 00000-0 21841-3 0 9993
2 25544 51.6426 254.8733 0008269 320.8811 145.3384 15.49640401381550
Epoch (UTC): | 06 February 2023 16:42:15 |
Eccentricity: | 0.0008269 |
inclination: | 51.6426° |
perigee height: | 412 km |
apogee height: | 423 km |
right ascension of ascending node: | 254.8733° |
argument of perigee: | 320.8811° |
revolutions per day: | 15.49640401 |
mean anomaly at epoch: | 145.3384° |
orbit number at epoch: | 38155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|