View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53494U 26145.32363267 +.00000000 +00000-0 +33452-3 0 00008
2 53494 97.4450 266.4191 0002984 119.3242 240.8283 15.05629491 09
| Epoch (UTC): | 25 May 2026 07:46:01 |
| Eccentricity: | 0.0002984 |
| inclination: | 97.4450° |
| perigee height: | 548 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 266.4191° |
| argument of perigee: | 119.3242° |
| revolutions per day: | 15.05629491 |
| mean anomaly at epoch: | 240.8283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|