View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59417U 26145.50570059 +.00000000 +00000-0 -25154-3 0 00009
2 59417 43.0036 335.4422 0000685 287.7568 72.3209 15.27609929 02
| Epoch (UTC): | 25 May 2026 12:08:12 |
| Eccentricity: | 0.0000685 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 335.4422° |
| argument of perigee: | 287.7568° |
| revolutions per day: | 15.27609929 |
| mean anomaly at epoch: | 72.3209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|