View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65602U 26145.46270003 +.00000000 +00000-0 +29504-3 0 00005
2 65602 97.4464 213.9673 0001572 134.2766 225.8591 15.05657584 08
| Epoch (UTC): | 25 May 2026 11:06:17 |
| Eccentricity: | 0.0001572 |
| inclination: | 97.4464° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.9673° |
| argument of perigee: | 134.2766° |
| revolutions per day: | 15.05657584 |
| mean anomaly at epoch: | 225.8591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|