View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66440U 26145.46856021 +.00000000 +00000-0 +47418-3 0 00000
2 66440 43.0035 200.7374 0001466 272.5475 87.5209 15.27590130 03
| Epoch (UTC): | 25 May 2026 11:14:43 |
| Eccentricity: | 0.0001466 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.7374° |
| argument of perigee: | 272.5475° |
| revolutions per day: | 15.27590130 |
| mean anomaly at epoch: | 87.5209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|