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 23273.47796296 .00037029 00000-0 66226-3 0 9993
2 25544 51.6412 167.0103 0005272 67.2346 294.7439 15.49622180418125
Epoch (UTC): | 30 September 2023 11:28:16 |
Eccentricity: | 0.0005272 |
inclination: | 51.6412° |
perigee height: | 414 km |
apogee height: | 421 km |
right ascension of ascending node: | 167.0103° |
argument of perigee: | 67.2346° |
revolutions per day: | 15.49622180 |
mean anomaly at epoch: | 294.7439° |
orbit number at epoch: | 41812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|