View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56893U 26145.32926573 +.00000000 +00000-0 -76303-4 0 00003
2 56893 43.0040 12.1833 0001064 253.0658 107.0077 15.27593018 05
| Epoch (UTC): | 25 May 2026 07:54:08 |
| Eccentricity: | 0.0001064 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.1833° |
| argument of perigee: | 253.0658° |
| revolutions per day: | 15.27593018 |
| mean anomaly at epoch: | 107.0077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|