View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 43476U 18047A 23029.63481479 +.00003298 00000-0 +13182-3 0 05
2 43476 88.9910 7.8899 0013572 195.1284 244.7943 15.24987544260886
Epoch (UTC): | 29 January 2023 15:14:07 |
Eccentricity: | 0.0013572 |
inclination: | 88.9910° |
perigee height: | 481 km |
apogee height: | 500 km |
right ascension of ascending node: | 7.8899° |
argument of perigee: | 195.1284° |
revolutions per day: | 15.24987544 |
mean anomaly at epoch: | 244.7943° |
orbit number at epoch: | 26088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|