View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43792U 26145.56283377 +.00000000 +00000-0 +94511-4 0 00001
2 43792 97.3994 183.9199 0013671 56.7493 303.5041 15.04169051 08
| Epoch (UTC): | 25 May 2026 13:30:28 |
| Eccentricity: | 0.0013671 |
| inclination: | 97.3994° |
| perigee height: | 545 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 183.9199° |
| argument of perigee: | 56.7493° |
| revolutions per day: | 15.04169051 |
| mean anomaly at epoch: | 303.5041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|