View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68526U 26145.38171789 +.00000000 +00000-0 +62976-3 0 00005
2 68526 53.1585 132.5735 0001147 87.0637 273.0500 15.42174911 08
| Epoch (UTC): | 25 May 2026 09:09:40 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.1585° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 132.5735° |
| argument of perigee: | 87.0637° |
| revolutions per day: | 15.42174911 |
| mean anomaly at epoch: | 273.0500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|