View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66478U 26145.58512065 +.00000000 +00000-0 +76092-3 0 00001
2 66478 43.0000 222.1522 0001533 274.8495 85.2182 15.27589514 00
| Epoch (UTC): | 25 May 2026 14:02:34 |
| Eccentricity: | 0.0001533 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.1522° |
| argument of perigee: | 274.8495° |
| revolutions per day: | 15.27589514 |
| mean anomaly at epoch: | 85.2182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|