View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25396U 26106.70242012 +.00000000 +00000-0 +49500-4 0 00003
2 25396 98.9850 96.2587 0002510 4.7368 355.3834 14.25741226 04
| Epoch (UTC): | 16 April 2026 16:51:29 |
| Eccentricity: | 0.0002510 |
| inclination: | 98.9850° |
| perigee height: | 804 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 96.2587° |
| argument of perigee: | 4.7368° |
| revolutions per day: | 14.25741226 |
| mean anomaly at epoch: | 355.3834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|