View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67656U 26145.53592179 +.00000000 +00000-0 +72808-3 0 00000
2 67656 97.2842 178.8479 0001037 115.1016 245.0335 15.33470668 09
| Epoch (UTC): | 25 May 2026 12:51:43 |
| Eccentricity: | 0.0001037 |
| inclination: | 97.2842° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.8479° |
| argument of perigee: | 115.1016° |
| revolutions per day: | 15.33470668 |
| mean anomaly at epoch: | 245.0335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|