View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00085U 61004C 23265.38683993 .00055011 00000-0 90423-2 0 9993
2 00085 38.7571 6.5062 0309283 233.6651 123.5181 14.42785532101325
Epoch (UTC): | 22 September 2023 09:17:02 |
Eccentricity: | 0.0309283 |
inclination: | 38.7571° |
perigee height: | 529 km |
apogee height: | 970 km |
right ascension of ascending node: | 6.5062° |
argument of perigee: | 233.6651° |
revolutions per day: | 14.42785532 |
mean anomaly at epoch: | 123.5181° |
orbit number at epoch: | 10132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|