View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56104U 26145.18641975 +.00000000 +00000-0 +17547-4 0 00006
2 56104 43.0046 89.2873 0001249 258.6636 101.4075 15.27569048 09
| Epoch (UTC): | 25 May 2026 04:28:26 |
| Eccentricity: | 0.0001249 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 89.2873° |
| argument of perigee: | 258.6636° |
| revolutions per day: | 15.27569048 |
| mean anomaly at epoch: | 101.4075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|