View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65920U 26145.36478000 +.00000000 +00000-0 +52467-3 0 00008
2 65920 53.1574 169.7986 0000966 71.4235 288.6870 15.30210385 05
| Epoch (UTC): | 25 May 2026 08:45:16 |
| Eccentricity: | 0.0000966 |
| inclination: | 53.1574° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.7986° |
| argument of perigee: | 71.4235° |
| revolutions per day: | 15.30210385 |
| mean anomaly at epoch: | 288.6870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|