View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 06155U 26039.30125454 +.00000000 +00000-0 +22366-3 0 00006
2 06155 35.0011 117.9668 0033150 123.3475 237.0406 14.77600042 07
| Epoch (UTC): | 08 February 2026 07:13:48 |
| Eccentricity: | 0.0033150 |
| inclination: | 35.0011° |
| perigee height: | 614 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 117.9668° |
| argument of perigee: | 123.3475° |
| revolutions per day: | 14.77600042 |
| mean anomaly at epoch: | 237.0406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|