View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67869U 26145.45303863 +.00000000 +00000-0 +31333-3 0 00005
2 67869 53.1581 205.9012 0000859 81.5670 278.5430 15.34401729 04
| Epoch (UTC): | 25 May 2026 10:52:22 |
| Eccentricity: | 0.0000859 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 205.9012° |
| argument of perigee: | 81.5670° |
| revolutions per day: | 15.34401729 |
| mean anomaly at epoch: | 278.5430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|