View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68841U 26145.45731453 +.00000000 +00000-0 +12314-2 0 00003
2 68841 97.2855 160.0498 0001251 0.5219 359.6033 15.49235885 08
| Epoch (UTC): | 25 May 2026 10:58:31 |
| Eccentricity: | 0.0001251 |
| inclination: | 97.2855° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.0498° |
| argument of perigee: | 0.5219° |
| revolutions per day: | 15.49235885 |
| mean anomaly at epoch: | 359.6033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|