View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41634U 26066.18264904 +.00000000 +00000-0 +11993-3 0 00001
2 41634 75.0007 112.0243 0008636 280.9573 79.0644 14.93223713 04
| Epoch (UTC): | 07 March 2026 04:23:00 |
| Eccentricity: | 0.0008636 |
| inclination: | 75.0007° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 112.0243° |
| argument of perigee: | 280.9573° |
| revolutions per day: | 14.93223713 |
| mean anomaly at epoch: | 79.0644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|