View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39498U 26145.52709845 +.00000000 +00000-0 +00000-0 0 00004
2 39498 0.0479 108.6418 0000564 254.9146 143.3189 1.00271396 07
| Epoch (UTC): | 25 May 2026 12:39:01 |
| Eccentricity: | 0.0000564 |
| inclination: | 0.0479° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 108.6418° |
| argument of perigee: | 254.9146° |
| revolutions per day: | 1.00271396 |
| mean anomaly at epoch: | 143.3189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|