View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48325U 26145.28966824 +.00000000 +00000-0 +33113-4 0 00003
2 48325 53.1607 104.9035 0001336 85.2381 274.8773 15.31705100 09
| Epoch (UTC): | 25 May 2026 06:57:07 |
| Eccentricity: | 0.0001336 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.9035° |
| argument of perigee: | 85.2381° |
| revolutions per day: | 15.31705100 |
| mean anomaly at epoch: | 274.8773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|