View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68747U 26145.58335647 +.00000000 +00000-0 -32341-1 0 00009
2 68747 97.2851 9.2553 0001433 105.0954 281.7749 15.54440974 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001433 |
| inclination: | 97.2851° |
| perigee height: | 403 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 9.2553° |
| argument of perigee: | 105.0954° |
| revolutions per day: | 15.54440974 |
| mean anomaly at epoch: | 281.7749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|