View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67346U 26145.07835691 +.00000000 +00000-0 +11371-2 0 00001
2 67346 43.0032 155.9226 0002180 258.2745 101.7862 15.27570257 00
| Epoch (UTC): | 25 May 2026 01:52:50 |
| Eccentricity: | 0.0002180 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 155.9226° |
| argument of perigee: | 258.2745° |
| revolutions per day: | 15.27570257 |
| mean anomaly at epoch: | 101.7862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|