View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67828U 26145.47336367 +.00000000 +00000-0 +70380-3 0 00002
2 67828 43.0006 193.7200 0002084 278.7006 81.3609 15.27592696 01
| Epoch (UTC): | 25 May 2026 11:21:38 |
| Eccentricity: | 0.0002084 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.7200° |
| argument of perigee: | 278.7006° |
| revolutions per day: | 15.27592696 |
| mean anomaly at epoch: | 81.3609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|