View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14450U 26053.24214248 +.00000000 +00000-0 +67589-4 0 00009
2 14450 82.9344 357.0955 0042114 324.4543 144.8990 13.76529475 01
| Epoch (UTC): | 22 February 2026 05:48:41 |
| Eccentricity: | 0.0042114 |
| inclination: | 82.9344° |
| perigee height: | 945 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 357.0955° |
| argument of perigee: | 324.4543° |
| revolutions per day: | 13.76529475 |
| mean anomaly at epoch: | 144.8990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|