View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66342U 26145.25832257 +.00000000 +00000-0 +60025-3 0 00002
2 66342 42.9987 140.1742 0000498 262.6828 97.3967 15.27589409 07
| Epoch (UTC): | 25 May 2026 06:11:59 |
| Eccentricity: | 0.0000498 |
| inclination: | 42.9987° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 140.1742° |
| argument of perigee: | 262.6828° |
| revolutions per day: | 15.27589409 |
| mean anomaly at epoch: | 97.3967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|