View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64893U 26145.63745573 +.00000000 +00000-0 +51901-3 0 00000
2 64893 97.4524 115.2675 0003464 255.7475 104.3383 15.34523685 06
| Epoch (UTC): | 25 May 2026 15:17:56 |
| Eccentricity: | 0.0003464 |
| inclination: | 97.4524° |
| perigee height: | 460 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 115.2675° |
| argument of perigee: | 255.7475° |
| revolutions per day: | 15.34523685 |
| mean anomaly at epoch: | 104.3383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|