View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14452U 26041.61497972 +.00000000 +00000-0 +67139-4 0 00007
2 14452 81.1622 124.9683 0089581 209.6272 149.9818 14.27240465 05
| Epoch (UTC): | 10 February 2026 14:45:34 |
| Eccentricity: | 0.0089581 |
| inclination: | 81.1622° |
| perigee height: | 737 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 124.9683° |
| argument of perigee: | 209.6272° |
| revolutions per day: | 14.27240465 |
| mean anomaly at epoch: | 149.9818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|