View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56120U 26145.49600375 +.00000000 +00000-0 -39082-5 0 00007
2 56120 43.0031 73.4877 0000578 244.8089 115.2703 15.27575461 00
| Epoch (UTC): | 25 May 2026 11:54:14 |
| Eccentricity: | 0.0000578 |
| inclination: | 43.0031° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 73.4877° |
| argument of perigee: | 244.8089° |
| revolutions per day: | 15.27575461 |
| mean anomaly at epoch: | 115.2703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|