View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57122U 26145.22410944 +.00000000 +00000-0 +12267-3 0 00005
2 57122 43.0008 209.6405 0001158 276.3628 83.7092 15.27556127 09
| Epoch (UTC): | 25 May 2026 05:22:43 |
| Eccentricity: | 0.0001158 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 209.6405° |
| argument of perigee: | 276.3628° |
| revolutions per day: | 15.27556127 |
| mean anomaly at epoch: | 83.7092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|