View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19119U 26073.57135022 +.00000000 +00000-0 +19449-3 0 00007
2 19119 71.0015 235.6597 0013377 244.4444 181.0463 14.15741377 04
| Epoch (UTC): | 14 March 2026 13:42:44 |
| Eccentricity: | 0.0013377 |
| inclination: | 71.0015° |
| perigee height: | 830 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 235.6597° |
| argument of perigee: | 244.4444° |
| revolutions per day: | 14.15741377 |
| mean anomaly at epoch: | 181.0463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|