View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66354U 26145.51357094 +.00000000 +00000-0 +58156-3 0 00007
2 66354 53.1589 235.9149 0001812 88.8789 271.2420 15.30211442 01
| Epoch (UTC): | 25 May 2026 12:19:32 |
| Eccentricity: | 0.0001812 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.9149° |
| argument of perigee: | 88.8789° |
| revolutions per day: | 15.30211442 |
| mean anomaly at epoch: | 271.2420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|