View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57904U 26144.99819882 +.00000000 +00000-0 +38278-4 0 00001
2 57904 43.0055 243.5132 0002390 268.2455 91.8123 15.27579769 02
| Epoch (UTC): | 24 May 2026 23:57:24 |
| Eccentricity: | 0.0002390 |
| inclination: | 43.0055° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 243.5132° |
| argument of perigee: | 268.2455° |
| revolutions per day: | 15.27579769 |
| mean anomaly at epoch: | 91.8123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|