View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64706U 26145.33793948 +.00000000 +00000-0 +81450-4 0 00002
2 64706 69.9998 121.1310 0004026 265.4666 94.6033 14.98337437 05
| Epoch (UTC): | 25 May 2026 08:06:37 |
| Eccentricity: | 0.0004026 |
| inclination: | 69.9998° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 121.1310° |
| argument of perigee: | 265.4666° |
| revolutions per day: | 14.98337437 |
| mean anomaly at epoch: | 94.6033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|