View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17567U 26041.23498139 +.00000000 +00000-0 +55538-4 0 00001
2 17567 82.5289 118.5681 0018047 356.6618 3.4475 14.86105838 04
| Epoch (UTC): | 10 February 2026 05:38:22 |
| Eccentricity: | 0.0018047 |
| inclination: | 82.5289° |
| perigee height: | 598 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 118.5681° |
| argument of perigee: | 356.6618° |
| revolutions per day: | 14.86105838 |
| mean anomaly at epoch: | 3.4475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|