View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00117U 26050.17404301 +.00000000 +00000-0 +61696-4 0 00007
2 00117 66.8124 292.8514 0075700 15.6123 344.7264 13.90176675 01
| Epoch (UTC): | 19 February 2026 04:10:37 |
| Eccentricity: | 0.0075700 |
| inclination: | 66.8124° |
| perigee height: | 873 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 292.8514° |
| argument of perigee: | 15.6123° |
| revolutions per day: | 13.90176675 |
| mean anomaly at epoch: | 344.7264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|