View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39086U 26145.62521946 +.00000000 +00000-0 +46370-4 0 00006
2 39086 98.5560 332.4784 0002016 27.7617 332.3674 14.32849621 09
| Epoch (UTC): | 25 May 2026 15:00:18 |
| Eccentricity: | 0.0002016 |
| inclination: | 98.5560° |
| perigee height: | 781 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 332.4784° |
| argument of perigee: | 27.7617° |
| revolutions per day: | 14.32849621 |
| mean anomaly at epoch: | 332.3674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|