View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66902U 26145.09290720 +.00000000 +00000-0 +41981-3 0 00009
2 66902 53.1598 29.1493 0001055 81.8141 278.2981 15.34395070 02
| Epoch (UTC): | 25 May 2026 02:13:47 |
| Eccentricity: | 0.0001055 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 29.1493° |
| argument of perigee: | 81.8141° |
| revolutions per day: | 15.34395070 |
| mean anomaly at epoch: | 278.2981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|