View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56526U 26145.44299270 +.00000000 +00000-0 +17313-4 0 00001
2 56526 43.0045 139.3934 0001975 274.2876 85.7750 15.27575451 06
| Epoch (UTC): | 25 May 2026 10:37:54 |
| Eccentricity: | 0.0001975 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.3934° |
| argument of perigee: | 274.2876° |
| revolutions per day: | 15.27575451 |
| mean anomaly at epoch: | 85.7750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|