View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62766U 26145.51948807 +.00000000 +00000-0 +66727-3 0 00001
2 62766 53.1572 324.9139 0000664 22.0075 338.0956 15.34409183 07
| Epoch (UTC): | 25 May 2026 12:28:03 |
| Eccentricity: | 0.0000664 |
| inclination: | 53.1572° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 324.9139° |
| argument of perigee: | 22.0075° |
| revolutions per day: | 15.34409183 |
| mean anomaly at epoch: | 338.0956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|