View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39440U 13066AA 24262.42843168 .00012255 00000-0 13853-2 0 9995
2 39440 97.8176 204.1870 0066684 330.9912 28.7603 14.85002334582167
| Epoch (UTC): | 18 September 2024 10:16:56 |
| Eccentricity: | 0.0066684 |
| inclination: | 97.8176° |
| perigee height: | 567 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 204.1870° |
| argument of perigee: | 330.9912° |
| revolutions per day: | 14.85002334 |
| mean anomaly at epoch: | 28.7603° |
| orbit number at epoch: | 58216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|