View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57606U 26145.03229735 +.00000000 +00000-0 +24057-4 0 00008
2 57606 43.0037 10.2981 0001267 276.4320 83.6388 15.27576214 00
| Epoch (UTC): | 25 May 2026 00:46:30 |
| Eccentricity: | 0.0001267 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.2981° |
| argument of perigee: | 276.4320° |
| revolutions per day: | 15.27576214 |
| mean anomaly at epoch: | 83.6388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|