View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14407U 26101.02611242 +.00000000 +00000-0 +10065-2 0 00001
2 14407 82.7648 303.9362 0041553 97.2534 263.3374 14.22591648 07
| Epoch (UTC): | 11 April 2026 00:37:36 |
| Eccentricity: | 0.0041553 |
| inclination: | 82.7648° |
| perigee height: | 787 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 303.9362° |
| argument of perigee: | 97.2534° |
| revolutions per day: | 14.22591648 |
| mean anomaly at epoch: | 263.3374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|