View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59609U 26144.83814622 +.00000000 +00000-0 +17797-3 0 00007
2 59609 42.9999 323.9592 0001423 267.1951 92.8737 15.27588097 05
| Epoch (UTC): | 24 May 2026 20:06:55 |
| Eccentricity: | 0.0001423 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 323.9592° |
| argument of perigee: | 267.1951° |
| revolutions per day: | 15.27588097 |
| mean anomaly at epoch: | 92.8737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|