View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55352U 26145.52055955 +.00000000 +00000-0 -15748-4 0 00007
2 55352 43.0007 226.1040 0001143 271.2479 88.8242 15.27572149 07
| Epoch (UTC): | 25 May 2026 12:29:36 |
| Eccentricity: | 0.0001143 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 226.1040° |
| argument of perigee: | 271.2479° |
| revolutions per day: | 15.27572149 |
| mean anomaly at epoch: | 88.8242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|