View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55829U 26145.37694878 +.00000000 +00000-0 -10612-3 0 00006
2 55829 87.8930 294.2922 0002029 86.3424 273.7938 13.14501825 05
| Epoch (UTC): | 25 May 2026 09:02:48 |
| Eccentricity: | 0.0002029 |
| inclination: | 87.8930° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2922° |
| argument of perigee: | 86.3424° |
| revolutions per day: | 13.14501825 |
| mean anomaly at epoch: | 273.7938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|