View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68145U 26145.53274897 +.00000000 +00000-0 +74718-3 0 00000
2 68145 97.2851 167.1826 0000702 107.1718 252.9602 15.33453566 00
| Epoch (UTC): | 25 May 2026 12:47:09 |
| Eccentricity: | 0.0000702 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.1826° |
| argument of perigee: | 107.1718° |
| revolutions per day: | 15.33453566 |
| mean anomaly at epoch: | 252.9602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|