View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56379U 26145.40240047 +.00000000 +00000-0 +23965-4 0 00001
2 56379 43.0050 124.5159 0001817 274.9129 85.1515 15.27577260 09
| Epoch (UTC): | 25 May 2026 09:39:27 |
| Eccentricity: | 0.0001817 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.5159° |
| argument of perigee: | 274.9129° |
| revolutions per day: | 15.27577260 |
| mean anomaly at epoch: | 85.1515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|