View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65334U 26145.39964896 +.00000000 +00000-0 +10993-3 0 00001
2 65334 53.1574 210.2784 0001085 84.4092 275.7033 15.30194117 02
| Epoch (UTC): | 25 May 2026 09:35:29 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.2784° |
| argument of perigee: | 84.4092° |
| revolutions per day: | 15.30194117 |
| mean anomaly at epoch: | 275.7033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|