View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43823U 26145.53783266 +.00000000 +00000-0 +00000-0 0 00001
2 43823 0.0506 114.8095 0002237 321.7388 128.4583 1.00271059 03
| Epoch (UTC): | 25 May 2026 12:54:28 |
| Eccentricity: | 0.0002237 |
| inclination: | 0.0506° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 114.8095° |
| argument of perigee: | 321.7388° |
| revolutions per day: | 1.00271059 |
| mean anomaly at epoch: | 128.4583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|