View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57185U 26145.60956093 +.00000000 +00000-0 +53756-3 0 00004
2 57185 97.5073 215.7664 0008105 148.6280 211.5449 15.38418543 01
| Epoch (UTC): | 25 May 2026 14:37:46 |
| Eccentricity: | 0.0008105 |
| inclination: | 97.5073° |
| perigee height: | 445 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 215.7664° |
| argument of perigee: | 148.6280° |
| revolutions per day: | 15.38418543 |
| mean anomaly at epoch: | 211.5449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|