View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66269U 26145.41247715 +.00000000 +00000-0 +66899-3 0 00002
2 66269 53.1586 194.0851 0001102 55.9026 304.2081 15.34405589 00
| Epoch (UTC): | 25 May 2026 09:53:58 |
| Eccentricity: | 0.0001102 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 194.0851° |
| argument of perigee: | 55.9026° |
| revolutions per day: | 15.34405589 |
| mean anomaly at epoch: | 304.2081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|