View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54750U 26145.60712794 +.00000000 +00000-0 +45121-3 0 00004
2 54750 34.9818 327.5407 0006798 286.9680 73.0292 15.31842053 08
| Epoch (UTC): | 25 May 2026 14:34:15 |
| Eccentricity: | 0.0006798 |
| inclination: | 34.9818° |
| perigee height: | 466 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 327.5407° |
| argument of perigee: | 286.9680° |
| revolutions per day: | 15.31842053 |
| mean anomaly at epoch: | 73.0292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|