View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58634U 26145.57511301 +.00000000 +00000-0 +19857-3 0 00003
2 58634 43.0036 352.5006 0001203 273.6239 86.4475 15.27574460 08
| Epoch (UTC): | 25 May 2026 13:48:09 |
| Eccentricity: | 0.0001203 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.5006° |
| argument of perigee: | 273.6239° |
| revolutions per day: | 15.27574460 |
| mean anomaly at epoch: | 86.4475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|