View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55454U 26145.32967557 +.00000000 +00000-0 +14224-4 0 00005
2 55454 43.0025 255.8450 0000993 274.5187 85.5552 15.27577273 09
| Epoch (UTC): | 25 May 2026 07:54:43 |
| Eccentricity: | 0.0000993 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 255.8450° |
| argument of perigee: | 274.5187° |
| revolutions per day: | 15.27577273 |
| mean anomaly at epoch: | 85.5552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|