View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27607U 26105.97976697 +.00000000 +00000-0 +67375-4 0 00001
2 27607 64.5524 321.4340 0075542 273.7912 85.4559 14.82909238 03
| Epoch (UTC): | 15 April 2026 23:30:51 |
| Eccentricity: | 0.0075542 |
| inclination: | 64.5524° |
| perigee height: | 567 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 321.4340° |
| argument of perigee: | 273.7912° |
| revolutions per day: | 14.82909238 |
| mean anomaly at epoch: | 85.4559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|