View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66008U 26145.62483154 +.00000000 +00000-0 +59402-3 0 00007
2 66008 53.1597 106.6205 0001518 101.5545 258.5626 15.30201992 04
| Epoch (UTC): | 25 May 2026 14:59:45 |
| Eccentricity: | 0.0001518 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.6205° |
| argument of perigee: | 101.5545° |
| revolutions per day: | 15.30201992 |
| mean anomaly at epoch: | 258.5626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|