View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40376U 26108.25112197 +.00000000 +00000-0 +63167-4 0 00005
2 40376 98.1301 116.1890 0001896 83.4580 276.6838 14.63385306 01
| Epoch (UTC): | 18 April 2026 06:01:36 |
| Eccentricity: | 0.0001896 |
| inclination: | 98.1301° |
| perigee height: | 681 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 116.1890° |
| argument of perigee: | 83.4580° |
| revolutions per day: | 14.63385306 |
| mean anomaly at epoch: | 276.6838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|