View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39159U 26145.41713459 +.00000000 +00000-0 +49163-4 0 00009
2 39159 98.3574 125.1498 0003900 182.6159 177.5001 14.23591557 02
| Epoch (UTC): | 25 May 2026 10:00:40 |
| Eccentricity: | 0.0003900 |
| inclination: | 98.3574° |
| perigee height: | 810 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 125.1498° |
| argument of perigee: | 182.6159° |
| revolutions per day: | 14.23591557 |
| mean anomaly at epoch: | 177.5001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|