View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43679U 26150.52739552 +.00000000 +00000-0 +41410-3 0 00007
2 43679 98.0519 3.4121 0001551 180.9141 179.2088 15.16834173 04
| Epoch (UTC): | 30 May 2026 12:39:26 |
| Eccentricity: | 0.0001551 |
| inclination: | 98.0519° |
| perigee height: | 514 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 3.4121° |
| argument of perigee: | 180.9141° |
| revolutions per day: | 15.16834173 |
| mean anomaly at epoch: | 179.2088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|