View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66185U 26145.58575036 +.00000000 +00000-0 +58740-3 0 00003
2 66185 53.1572 248.3148 0000412 257.8014 102.2941 15.30188228 02
| Epoch (UTC): | 25 May 2026 14:03:28 |
| Eccentricity: | 0.0000412 |
| inclination: | 53.1572° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.3148° |
| argument of perigee: | 257.8014° |
| revolutions per day: | 15.30188228 |
| mean anomaly at epoch: | 102.2941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|