View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23179U 26053.67077926 +.00000000 +00000-0 +33694-4 0 00004
2 23179 82.9453 112.1001 0036228 51.9229 66.9665 13.76802105 01
| Epoch (UTC): | 22 February 2026 16:05:55 |
| Eccentricity: | 0.0036228 |
| inclination: | 82.9453° |
| perigee height: | 949 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 112.1001° |
| argument of perigee: | 51.9229° |
| revolutions per day: | 13.76802105 |
| mean anomaly at epoch: | 66.9665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|