View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56757U 26144.87590755 +.00000000 +00000-0 +00000-0 0 00006
2 56757 0.0812 32.0238 0004940 347.3899 204.3756 1.00271605 00
| Epoch (UTC): | 24 May 2026 21:01:18 |
| Eccentricity: | 0.0004940 |
| inclination: | 0.0812° |
| perigee height: | 35766 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 32.0238° |
| argument of perigee: | 347.3899° |
| revolutions per day: | 1.00271605 |
| mean anomaly at epoch: | 204.3756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|