View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56388U 26145.37812941 +.00000000 +00000-0 +21493-4 0 00009
2 56388 43.0014 125.1702 0000237 237.6034 122.4795 15.27576561 04
| Epoch (UTC): | 25 May 2026 09:04:30 |
| Eccentricity: | 0.0000237 |
| inclination: | 43.0014° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 125.1702° |
| argument of perigee: | 237.6034° |
| revolutions per day: | 15.27576561 |
| mean anomaly at epoch: | 122.4795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|