View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66024U 26145.19389699 +.00000000 +00000-0 +58403-3 0 00006
2 66024 53.1549 108.1962 0000973 54.9913 305.1179 15.30196866 05
| Epoch (UTC): | 25 May 2026 04:39:12 |
| Eccentricity: | 0.0000973 |
| inclination: | 53.1549° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.1962° |
| argument of perigee: | 54.9913° |
| revolutions per day: | 15.30196866 |
| mean anomaly at epoch: | 305.1179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|