View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54650U 26145.58547095 +.00000000 +00000-0 -17835-3 0 00002
2 54650 87.9252 248.4946 0002094 98.9514 261.1857 13.21825189 03
| Epoch (UTC): | 25 May 2026 14:03:04 |
| Eccentricity: | 0.0002094 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4946° |
| argument of perigee: | 98.9514° |
| revolutions per day: | 13.21825189 |
| mean anomaly at epoch: | 261.1857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|