View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67174U 26145.51790034 +.00000000 +00000-0 +61915-3 0 00000
2 67174 43.0010 236.9501 0002098 279.5542 80.5072 15.27591579 07
| Epoch (UTC): | 25 May 2026 12:25:46 |
| Eccentricity: | 0.0002098 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.9501° |
| argument of perigee: | 279.5542° |
| revolutions per day: | 15.27591579 |
| mean anomaly at epoch: | 80.5072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|