View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67065U 26145.62785773 +.00000000 +00000-0 +90519-4 0 00008
2 67065 49.9979 106.1788 0000848 354.1816 5.9046 13.29326254 03
| Epoch (UTC): | 25 May 2026 15:04:06 |
| Eccentricity: | 0.0000848 |
| inclination: | 49.9979° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 106.1788° |
| argument of perigee: | 354.1816° |
| revolutions per day: | 13.29326254 |
| mean anomaly at epoch: | 5.9046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|