View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64747U 26145.47388080 +.00000000 +00000-0 +28274-3 0 00003
2 64747 53.1587 171.8374 0001108 92.9757 267.1370 15.30204342 09
| Epoch (UTC): | 25 May 2026 11:22:23 |
| Eccentricity: | 0.0001108 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.8374° |
| argument of perigee: | 92.9757° |
| revolutions per day: | 15.30204342 |
| mean anomaly at epoch: | 267.1370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|