View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40254U 97082P 24356.07300935 .00058277 00000-0 18447-1 0 9992
2 40254 86.0112 118.0072 0127165 176.0955 184.1266 14.35238172523519
| Epoch (UTC): | 21 December 2024 01:45:08 |
| Eccentricity: | 0.0127165 |
| inclination: | 86.0112° |
| perigee height: | 683 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 118.0072° |
| argument of perigee: | 176.0955° |
| revolutions per day: | 14.35238172 |
| mean anomaly at epoch: | 184.1266° |
| orbit number at epoch: | 52351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|