View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68314U 26145.31984451 +.00000000 +00000-0 +85418-3 0 00007
2 68314 97.2854 271.6539 0001275 22.5120 337.6201 15.75195171 03
| Epoch (UTC): | 25 May 2026 07:40:34 |
| Eccentricity: | 0.0001275 |
| inclination: | 97.2854° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6539° |
| argument of perigee: | 22.5120° |
| revolutions per day: | 15.75195171 |
| mean anomaly at epoch: | 337.6201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|