View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33446U 26113.38512985 +.00000000 +00000-0 +95579-4 0 00006
2 33446 97.9286 47.3120 0012878 247.3991 112.5861 14.83093955 02
| Epoch (UTC): | 23 April 2026 09:14:35 |
| Eccentricity: | 0.0012878 |
| inclination: | 97.9286° |
| perigee height: | 611 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 47.3120° |
| argument of perigee: | 247.3991° |
| revolutions per day: | 14.83093955 |
| mean anomaly at epoch: | 112.5861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|