View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67340U 26145.38598856 +.00000000 +00000-0 +47144-3 0 00006
2 67340 43.0009 153.9238 0001418 276.1177 83.9513 15.27591590 07
| Epoch (UTC): | 25 May 2026 09:15:49 |
| Eccentricity: | 0.0001418 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.9238° |
| argument of perigee: | 276.1177° |
| revolutions per day: | 15.27591590 |
| mean anomaly at epoch: | 83.9513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|