View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55163U 26145.12880757 +.00000000 +00000-0 +90917-3 0 00008
2 55163 87.8917 25.6542 0002109 102.1112 258.0252 13.11414083 06
| Epoch (UTC): | 25 May 2026 03:05:28 |
| Eccentricity: | 0.0002109 |
| inclination: | 87.8917° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6542° |
| argument of perigee: | 102.1112° |
| revolutions per day: | 13.11414083 |
| mean anomaly at epoch: | 258.0252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|