View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57331U 26145.55714449 +.00000000 +00000-0 +30098-4 0 00003
2 57331 43.0026 178.1832 0001917 281.5161 78.5475 15.27576898 02
| Epoch (UTC): | 25 May 2026 13:22:17 |
| Eccentricity: | 0.0001917 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.1832° |
| argument of perigee: | 281.5161° |
| revolutions per day: | 15.27576898 |
| mean anomaly at epoch: | 78.5475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|