View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63593U 26145.26649666 +.00000000 +00000-0 +46387-3 0 00003
2 63593 43.0001 249.0680 0000848 278.1618 81.9138 15.27589396 03
| Epoch (UTC): | 25 May 2026 06:23:45 |
| Eccentricity: | 0.0000848 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 249.0680° |
| argument of perigee: | 278.1618° |
| revolutions per day: | 15.27589396 |
| mean anomaly at epoch: | 81.9138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|