View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64029U 26145.41924652 +.00000000 +00000-0 +24814-3 0 00007
2 64029 70.0011 281.0606 0002747 261.7954 98.2894 14.98336585 01
| Epoch (UTC): | 25 May 2026 10:03:42 |
| Eccentricity: | 0.0002747 |
| inclination: | 70.0011° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.0606° |
| argument of perigee: | 261.7954° |
| revolutions per day: | 14.98336585 |
| mean anomaly at epoch: | 98.2894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|