View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39719U 92093KK 24354.13721390 .00000241 00000-0 19879-3 0 9990
2 39719 71.2986 256.5512 0097954 350.6952 78.1671 13.96082043543765
| Epoch (UTC): | 19 December 2024 03:17:35 |
| Eccentricity: | 0.0097954 |
| inclination: | 71.2986° |
| perigee height: | 836 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 256.5512° |
| argument of perigee: | 350.6952° |
| revolutions per day: | 13.96082043 |
| mean anomaly at epoch: | 78.1671° |
| orbit number at epoch: | 54376 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|