View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65793U 26145.12170877 +.00000000 +00000-0 +41234-3 0 00001
2 65793 97.4522 7.9583 0002012 101.1159 259.0295 15.05661673 08
| Epoch (UTC): | 25 May 2026 02:55:15 |
| Eccentricity: | 0.0002012 |
| inclination: | 97.4522° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 7.9583° |
| argument of perigee: | 101.1159° |
| revolutions per day: | 15.05661673 |
| mean anomaly at epoch: | 259.0295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|