View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19119U 26066.79300375 +.00000000 +00000-0 +15227-4 0 00009
2 19119 71.0005 249.9114 0013616 253.3180 195.5585 14.15738451 02
| Epoch (UTC): | 07 March 2026 19:01:55 |
| Eccentricity: | 0.0013616 |
| inclination: | 71.0005° |
| perigee height: | 830 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 249.9114° |
| argument of perigee: | 253.3180° |
| revolutions per day: | 14.15738451 |
| mean anomaly at epoch: | 195.5585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|