View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26609U 00072B 23087.75656694 -.00000338 00000-0 00000-0 0 9995
2 26609 5.7492 196.8370 7936289 139.6422 319.4364 1.25588702102727
| Epoch (UTC): | 28 March 2023 18:09:27 |
| Eccentricity: | 0.7936289 |
| inclination: | 5.7492° |
| perigee height: | 1111 km |
| apogee height: | 58709 km |
| right ascension of ascending node: | 196.8370° |
| argument of perigee: | 139.6422° |
| revolutions per day: | 1.25588702 |
| mean anomaly at epoch: | 319.4364° |
| orbit number at epoch: | 10272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|