View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67917U 26145.44008168 +.00000000 +00000-0 +36747-3 0 00002
2 67917 43.0014 171.4930 0001560 282.6944 77.3734 15.27586983 01
| Epoch (UTC): | 25 May 2026 10:33:43 |
| Eccentricity: | 0.0001560 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.4930° |
| argument of perigee: | 282.6944° |
| revolutions per day: | 15.27586983 |
| mean anomaly at epoch: | 77.3734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|