View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47384U 26145.41744865 +.00000000 +00000-0 +11520-4 0 00009
2 47384 53.1571 40.2932 0001365 83.2678 276.8477 15.29357096 07
| Epoch (UTC): | 25 May 2026 10:01:07 |
| Eccentricity: | 0.0001365 |
| inclination: | 53.1571° |
| perigee height: | 477 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 40.2932° |
| argument of perigee: | 83.2678° |
| revolutions per day: | 15.29357096 |
| mean anomaly at epoch: | 276.8477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|