View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51743U 26145.48416176 +.00000000 +00000-0 +14107-4 0 00005
2 51743 53.2120 324.3013 0001176 85.5128 274.5998 15.08835675 07
| Epoch (UTC): | 25 May 2026 11:37:11 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 324.3013° |
| argument of perigee: | 85.5128° |
| revolutions per day: | 15.08835675 |
| mean anomaly at epoch: | 274.5998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|