View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67962U 26145.48066279 +.00000000 +00000-0 +90824-3 0 00009
2 67962 97.2833 155.4404 0001442 99.3257 260.8148 15.33461317 06
| Epoch (UTC): | 25 May 2026 11:32:09 |
| Eccentricity: | 0.0001442 |
| inclination: | 97.2833° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4404° |
| argument of perigee: | 99.3257° |
| revolutions per day: | 15.33461317 |
| mean anomaly at epoch: | 260.8148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|