View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40484U 26145.58335647 +.00000000 +00000-0 +00000-0 0 00002
2 40484 71.8326 349.1071 8341288 166.9223 152.7239 0.28352380 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.8341288 |
| inclination: | 71.8326° |
| perigee height: | 9857 km |
| apogee height: | 173139 km |
| right ascension of ascending node: | 349.1071° |
| argument of perigee: | 166.9223° |
| revolutions per day: | 0.28352380 |
| mean anomaly at epoch: | 152.7239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|