View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54831U 26145.12678591 +.00000000 +00000-0 +26520-4 0 00000
2 54831 43.0034 64.3602 0001224 240.5490 119.5239 15.27578250 03
| Epoch (UTC): | 25 May 2026 03:02:34 |
| Eccentricity: | 0.0001224 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.3602° |
| argument of perigee: | 240.5490° |
| revolutions per day: | 15.27578250 |
| mean anomaly at epoch: | 119.5239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|