View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40483U 26145.58335647 +.00000000 +00000-0 +00000-0 0 00001
2 40483 71.8296 349.1026 8342085 166.9278 152.7255 0.28352411 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.8342085 |
| inclination: | 71.8296° |
| perigee height: | 9849 km |
| apogee height: | 173146 km |
| right ascension of ascending node: | 349.1026° |
| argument of perigee: | 166.9278° |
| revolutions per day: | 0.28352411 |
| mean anomaly at epoch: | 152.7255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|