View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66433U 26145.44800351 +.00000000 +00000-0 +52697-3 0 00000
2 66433 43.0004 200.5813 0001243 278.5985 81.4725 15.27591780 00
| Epoch (UTC): | 25 May 2026 10:45:07 |
| Eccentricity: | 0.0001243 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.5813° |
| argument of perigee: | 278.5985° |
| revolutions per day: | 15.27591780 |
| mean anomaly at epoch: | 81.4725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|