View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64580U 26145.27243494 +.00000000 +00000-0 +17581-3 0 00004
2 64580 97.7705 259.4475 0004550 77.8760 282.2968 14.91719739 03
| Epoch (UTC): | 25 May 2026 06:32:18 |
| Eccentricity: | 0.0004550 |
| inclination: | 97.7705° |
| perigee height: | 589 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 259.4475° |
| argument of perigee: | 77.8760° |
| revolutions per day: | 14.91719739 |
| mean anomaly at epoch: | 282.2968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|