View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 34903U 09023A 22254.93773514 0.00000000 00000-0 00000-0 0 00
2 34903 98.9147 351.9643 0009053 297.6170 62.3707 14.06662686 09
Epoch (UTC): | 11 September 2022 22:30:20 |
Eccentricity: | 0.0009053 |
inclination: | 98.9147° |
perigee height: | 864 km |
apogee height: | 877 km |
right ascension of ascending node: | 351.9643° |
argument of perigee: | 297.6170° |
revolutions per day: | 14.06662686 |
mean anomaly at epoch: | 62.3707° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|