View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10967U 26162.22192905 +.00000000 +00000-0 +99872-4 0 00002
2 10967 108.0166 321.7670 0001985 240.7099 119.3848 14.46238733 02
| Epoch (UTC): | 11 June 2026 05:19:34 |
| Eccentricity: | 0.0001985 |
| inclination: | 108.0166° |
| perigee height: | 737 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 321.7670° |
| argument of perigee: | 240.7099° |
| revolutions per day: | 14.46238733 |
| mean anomaly at epoch: | 119.3848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|