View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00045U 60007A 23337.31664289 .00000567 00000-0 16918-3 0 9995
2 00045 66.6944 289.1200 0246509 116.1679 246.5000 14.34457883247035
Epoch (UTC): | 03 December 2023 07:35:57 |
Eccentricity: | 0.0246509 |
inclination: | 66.6944° |
perigee height: | 600 km |
apogee height: | 953 km |
right ascension of ascending node: | 289.1200° |
argument of perigee: | 116.1679° |
revolutions per day: | 14.34457883 |
mean anomaly at epoch: | 246.5000° |
orbit number at epoch: | 24703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|