View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48674U 26145.32969899 +.00000000 +00000-0 -51105-5 0 00003
2 48674 53.1614 117.9600 0001218 92.2565 267.8575 15.29350962 08
| Epoch (UTC): | 25 May 2026 07:54:45 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.1614° |
| perigee height: | 477 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 117.9600° |
| argument of perigee: | 92.2565° |
| revolutions per day: | 15.29350962 |
| mean anomaly at epoch: | 267.8575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|