View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40076U 26144.94676020 +.00000000 +00000-0 +42091-3 0 00000
2 40076 98.3814 134.8649 0006094 4.9095 355.2192 15.12872787 08
| Epoch (UTC): | 24 May 2026 22:43:20 |
| Eccentricity: | 0.0006094 |
| inclination: | 98.3814° |
| perigee height: | 523 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 134.8649° |
| argument of perigee: | 4.9095° |
| revolutions per day: | 15.12872787 |
| mean anomaly at epoch: | 355.2192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|