View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 107U 61013A 24280.21560440 .00006348 00000-0 79070-3 0 9994
2 107 28.7856 273.1620 0515346 127.3070 237.5616 14.16853000187993
Epoch (UTC): | 06 October 2024 05:10:28 |
Eccentricity: | 0.0515346 |
inclination: | 28.7856° |
perigee height: | 464 km |
apogee height: | 1208 km |
right ascension of ascending node: | 273.1620° |
argument of perigee: | 127.3070° |
revolutions per day: | 14.16853000 |
mean anomaly at epoch: | 237.5616° |
orbit number at epoch: | 18799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|