View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43603U 26142.80695774 +.00000000 +00000-0 +00000-0 0 00000
2 43603 54.1759 181.8646 0004460 15.0351 345.0417 1.86227142 09
| Epoch (UTC): | 22 May 2026 19:22:01 |
| Eccentricity: | 0.0004460 |
| inclination: | 54.1759° |
| perigee height: | 21516 km |
| apogee height: | 21541 km |
| right ascension of ascending node: | 181.8646° |
| argument of perigee: | 15.0351° |
| revolutions per day: | 1.86227142 |
| mean anomaly at epoch: | 345.0417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|