View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57747U 26144.92484785 +.00000000 +00000-0 +37560-4 0 00002
2 57747 43.0027 102.0834 0001046 267.4479 92.6253 15.27576726 01
| Epoch (UTC): | 24 May 2026 22:11:46 |
| Eccentricity: | 0.0001046 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 102.0834° |
| argument of perigee: | 267.4479° |
| revolutions per day: | 15.27576726 |
| mean anomaly at epoch: | 92.6253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|