View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66368U 26145.54035907 +.00000000 +00000-0 +16599-3 0 00006
2 66368 53.1593 233.1883 0000846 54.8961 305.2119 15.30195595 00
| Epoch (UTC): | 25 May 2026 12:58:07 |
| Eccentricity: | 0.0000846 |
| inclination: | 53.1593° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.1883° |
| argument of perigee: | 54.8961° |
| revolutions per day: | 15.30195595 |
| mean anomaly at epoch: | 305.2119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|