View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67667U 26145.50871484 +.00000000 +00000-0 +68151-3 0 00004
2 67667 97.2851 178.7307 0000583 179.4544 180.6700 15.33452464 08
| Epoch (UTC): | 25 May 2026 12:12:32 |
| Eccentricity: | 0.0000583 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.7307° |
| argument of perigee: | 179.4544° |
| revolutions per day: | 15.33452464 |
| mean anomaly at epoch: | 180.6700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|