View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39483U 26145.57945735 +.00000000 +00000-0 -45198-3 0 00004
2 39483 82.4846 182.7808 0020437 142.1839 218.0681 12.42904693 05
| Epoch (UTC): | 25 May 2026 13:54:25 |
| Eccentricity: | 0.0020437 |
| inclination: | 82.4846° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 182.7808° |
| argument of perigee: | 142.1839° |
| revolutions per day: | 12.42904693 |
| mean anomaly at epoch: | 218.0681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|