View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39035U 26145.56102166 +.00000000 +00000-0 +00000-0 0 00008
2 39035 0.0383 112.0873 0001651 336.6070 241.5957 1.00271977 03
| Epoch (UTC): | 25 May 2026 13:27:52 |
| Eccentricity: | 0.0001651 |
| inclination: | 0.0383° |
| perigee height: | 35780 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 112.0873° |
| argument of perigee: | 336.6070° |
| revolutions per day: | 1.00271977 |
| mean anomaly at epoch: | 241.5957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|