View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32265U 26145.35342515 +.00000000 +00000-0 +20886-3 0 00004
2 32265 51.9563 123.4604 0005013 353.5505 172.7554 12.30388876 01
| Epoch (UTC): | 25 May 2026 08:28:55 |
| Eccentricity: | 0.0005013 |
| inclination: | 51.9563° |
| perigee height: | 1544 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 123.4604° |
| argument of perigee: | 353.5505° |
| revolutions per day: | 12.30388876 |
| mean anomaly at epoch: | 172.7554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|