View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67468U 26145.24506284 +.00000000 +00000-0 +97011-3 0 00004
2 67468 42.9994 132.5810 0000823 258.7571 101.3188 15.27600834 06
| Epoch (UTC): | 25 May 2026 05:52:53 |
| Eccentricity: | 0.0000823 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.5810° |
| argument of perigee: | 258.7571° |
| revolutions per day: | 15.27600834 |
| mean anomaly at epoch: | 101.3188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|