View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62198U 26145.58437269 +.00000000 +00000-0 +61227-3 0 00002
2 62198 43.0012 196.2660 0002127 272.3787 87.6821 15.27589113 00
| Epoch (UTC): | 25 May 2026 14:01:29 |
| Eccentricity: | 0.0002127 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.2660° |
| argument of perigee: | 272.3787° |
| revolutions per day: | 15.27589113 |
| mean anomaly at epoch: | 87.6821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|