View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64475U 26145.19202123 +.00000000 +00000-0 +62655-3 0 00004
2 64475 53.1605 119.1561 0000715 72.9715 287.1366 15.35411245 00
| Epoch (UTC): | 25 May 2026 04:36:30 |
| Eccentricity: | 0.0000715 |
| inclination: | 53.1605° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 119.1561° |
| argument of perigee: | 72.9715° |
| revolutions per day: | 15.35411245 |
| mean anomaly at epoch: | 287.1366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|