View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53684U 26145.38043851 +.00000000 +00000-0 +14262-2 0 00006
2 53684 97.4462 25.3168 0002461 95.5611 264.5897 15.05544925 06
| Epoch (UTC): | 25 May 2026 09:07:49 |
| Eccentricity: | 0.0002461 |
| inclination: | 97.4462° |
| perigee height: | 548 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 25.3168° |
| argument of perigee: | 95.5611° |
| revolutions per day: | 15.05544925 |
| mean anomaly at epoch: | 264.5897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|