View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58224U 26145.40027517 +.00000000 +00000-0 +26182-3 0 00000
2 58224 43.0013 120.7901 0001979 275.6926 84.3700 15.27589774 04
| Epoch (UTC): | 25 May 2026 09:36:23 |
| Eccentricity: | 0.0001979 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.7901° |
| argument of perigee: | 275.6926° |
| revolutions per day: | 15.27589774 |
| mean anomaly at epoch: | 84.3700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|