View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68296U 26145.33335647 +.00000000 +00000-0 +19493-3 0 00005
2 68296 97.2838 271.5626 0001465 77.4208 103.3021 15.75167680 09
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001465 |
| inclination: | 97.2838° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.5626° |
| argument of perigee: | 77.4208° |
| revolutions per day: | 15.75167680 |
| mean anomaly at epoch: | 103.3021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|