View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43806U 26088.07586240 +.00000000 +00000-0 +39654-3 0 00000
2 43806 97.4094 137.5257 0005999 239.1380 120.9263 15.14982536 01
| Epoch (UTC): | 29 March 2026 01:49:14 |
| Eccentricity: | 0.0005999 |
| inclination: | 97.4094° |
| perigee height: | 517 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 137.5257° |
| argument of perigee: | 239.1380° |
| revolutions per day: | 15.14982536 |
| mean anomaly at epoch: | 120.9263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|