View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43476U 18047A 26074.08550922 +.00005752 00000-0 +15577-3 0 04
2 43476 88.9913 210.8714 0013783 115.1224 324.4540 15.37515384435348
| Epoch (UTC): | 15 March 2026 02:03:07 |
| Eccentricity: | 0.0013783 |
| inclination: | 88.9913° |
| perigee height: | 444 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 210.8714° |
| argument of perigee: | 115.1224° |
| revolutions per day: | 15.37515384 |
| mean anomaly at epoch: | 324.4540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|