View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19649U 26021.49133582 +.00000000 +00000-0 +19523-3 0 00001
2 19649 71.0014 313.2420 0007269 233.5711 126.4742 14.15188401 04
| Epoch (UTC): | 21 January 2026 11:47:31 |
| Eccentricity: | 0.0007269 |
| inclination: | 71.0014° |
| perigee height: | 836 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 313.2420° |
| argument of perigee: | 233.5711° |
| revolutions per day: | 14.15188401 |
| mean anomaly at epoch: | 126.4742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|