View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67431U 26145.41663987 +.00000000 +00000-0 +37598-3 0 00001
2 67431 42.9998 164.4227 0001320 272.3675 87.7025 15.27589012 07
| Epoch (UTC): | 25 May 2026 09:59:57 |
| Eccentricity: | 0.0001320 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.4227° |
| argument of perigee: | 272.3675° |
| revolutions per day: | 15.27589012 |
| mean anomaly at epoch: | 87.7025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|