View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43651U 26146.14063020 +.00000000 +00000-0 +00000-0 0 00007
2 43651 1.4286 2.1161 0062049 357.3116 227.3494 1.00268501 04
| Epoch (UTC): | 26 May 2026 03:22:30 |
| Eccentricity: | 0.0062049 |
| inclination: | 1.4286° |
| perigee height: | 35526 km |
| apogee height: | 36049 km |
| right ascension of ascending node: | 2.1161° |
| argument of perigee: | 357.3116° |
| revolutions per day: | 1.00268501 |
| mean anomaly at epoch: | 227.3494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|