View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64616U 26145.51912712 +.00000000 +00000-0 +59128-3 0 00000
2 64616 53.1600 338.6673 0001410 61.1742 298.9400 15.30208965 04
| Epoch (UTC): | 25 May 2026 12:27:32 |
| Eccentricity: | 0.0001410 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.6673° |
| argument of perigee: | 61.1742° |
| revolutions per day: | 15.30208965 |
| mean anomaly at epoch: | 298.9400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|