View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54689U 26145.63485109 +.00000000 +00000-0 +30407-3 0 00006
2 54689 97.6930 314.8299 0005185 178.1222 182.0040 15.33919684 00
| Epoch (UTC): | 25 May 2026 15:14:11 |
| Eccentricity: | 0.0005185 |
| inclination: | 97.6930° |
| perigee height: | 461 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 314.8299° |
| argument of perigee: | 178.1222° |
| revolutions per day: | 15.33919684 |
| mean anomaly at epoch: | 182.0040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|