View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56399U 26145.36404353 +.00000000 +00000-0 -27532-4 0 00005
2 56399 43.0051 113.7958 0001278 353.5720 6.5115 15.27560045 07
| Epoch (UTC): | 25 May 2026 08:44:13 |
| Eccentricity: | 0.0001278 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.7958° |
| argument of perigee: | 353.5720° |
| revolutions per day: | 15.27560045 |
| mean anomaly at epoch: | 6.5115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|