View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27386U 02009A 24312.84718076 .00000803 00000-0 27519-3 0 9998
2 27386 98.3032 269.0877 0001354 83.0172 308.1475 14.38750040189161
Epoch (UTC): | 07 November 2024 20:19:56 |
Eccentricity: | 0.0001354 |
inclination: | 98.3032° |
perigee height: | 761 km |
apogee height: | 763 km |
right ascension of ascending node: | 269.0877° |
argument of perigee: | 83.0172° |
revolutions per day: | 14.38750040 |
mean anomaly at epoch: | 308.1475° |
orbit number at epoch: | 18916 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|