View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40039U 26145.35558444 +.00000000 +00000-0 +10539-3 0 00006
2 40039 97.9634 89.1158 0012171 20.0690 340.1006 14.95542388 00
| Epoch (UTC): | 25 May 2026 08:32:02 |
| Eccentricity: | 0.0012171 |
| inclination: | 97.9634° |
| perigee height: | 572 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 89.1158° |
| argument of perigee: | 20.0690° |
| revolutions per day: | 14.95542388 |
| mean anomaly at epoch: | 340.1006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|