View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17070U 26053.80951972 +.00000000 +00000-0 +11084-3 0 00002
2 17070 89.6240 180.9036 0037331 262.4627 256.5431 13.75266943 01
| Epoch (UTC): | 22 February 2026 19:25:42 |
| Eccentricity: | 0.0037331 |
| inclination: | 89.6240° |
| perigee height: | 953 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 180.9036° |
| argument of perigee: | 262.4627° |
| revolutions per day: | 13.75266943 |
| mean anomaly at epoch: | 256.5431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|