View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40384U 26145.50135832 +.00000000 +00000-0 +00000-0 0 00007
2 40384 0.0162 338.7631 0001376 204.4481 185.3263 1.00272723 03
| Epoch (UTC): | 25 May 2026 12:01:57 |
| Eccentricity: | 0.0001376 |
| inclination: | 0.0162° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 338.7631° |
| argument of perigee: | 204.4481° |
| revolutions per day: | 1.00272723 |
| mean anomaly at epoch: | 185.3263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|