View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39484U 26160.12425764 +.00000000 +00000-0 -86793-3 0 00004
2 39484 82.4870 175.0948 0022574 111.9787 248.3694 12.42878874 04
| Epoch (UTC): | 09 June 2026 02:58:55 |
| Eccentricity: | 0.0022574 |
| inclination: | 82.4870° |
| perigee height: | 1477 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 175.0948° |
| argument of perigee: | 111.9787° |
| revolutions per day: | 12.42878874 |
| mean anomaly at epoch: | 248.3694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|