View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40267U 26063.58768698 +.00000000 +00000-0 +00000-0 0 00006
2 40267 0.0312 247.5940 0000766 82.9448 184.0089 1.00271913 06
| Epoch (UTC): | 04 March 2026 14:06:16 |
| Eccentricity: | 0.0000766 |
| inclination: | 0.0312° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 247.5940° |
| argument of perigee: | 82.9448° |
| revolutions per day: | 1.00271913 |
| mean anomaly at epoch: | 184.0089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|