View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68405U 26145.72727161 +.00000000 +00000-0 +18773-3 0 00006
2 68405 97.4626 221.3605 0014624 32.5508 327.6627 15.23681980 04
| Epoch (UTC): | 25 May 2026 17:27:16 |
| Eccentricity: | 0.0014624 |
| inclination: | 97.4626° |
| perigee height: | 485 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 221.3605° |
| argument of perigee: | 32.5508° |
| revolutions per day: | 15.23681980 |
| mean anomaly at epoch: | 327.6627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|