View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57358U 26145.66668980 +.00000000 +00000-0 -12826-3 0 00001
2 57358 43.0021 166.5454 0001447 287.1885 188.6250 15.27588013 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001447 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 166.5454° |
| argument of perigee: | 287.1885° |
| revolutions per day: | 15.27588013 |
| mean anomaly at epoch: | 188.6250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|