View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39266U 26032.47450690 +.00000000 +00000-0 +44451-3 0 00008
2 39266 80.9390 161.3658 0165042 299.1166 59.3649 15.63897000 04
| Epoch (UTC): | 01 February 2026 11:23:17 |
| Eccentricity: | 0.0165042 |
| inclination: | 80.9390° |
| perigee height: | 265 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 161.3658° |
| argument of perigee: | 299.1166° |
| revolutions per day: | 15.63897000 |
| mean anomaly at epoch: | 59.3649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|