View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27422U 02021B 23273.78475791 .00000532 00000-0 22363-3 0 9996
2 27422 98.4971 212.1318 0011083 294.4218 65.5807 14.29793970114758
| Epoch (UTC): | 30 September 2023 18:50:03 |
| Eccentricity: | 0.0011083 |
| inclination: | 98.4971° |
| perigee height: | 784 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 212.1318° |
| argument of perigee: | 294.4218° |
| revolutions per day: | 14.29793970 |
| mean anomaly at epoch: | 65.5807° |
| orbit number at epoch: | 11475 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|