View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46488U 26145.60941594 +.00000000 +00000-0 +18736-3 0 00007
2 46488 82.4983 1.1232 0014445 94.7530 265.5200 12.42891413 06
| Epoch (UTC): | 25 May 2026 14:37:33 |
| Eccentricity: | 0.0014445 |
| inclination: | 82.4983° |
| perigee height: | 1483 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 1.1232° |
| argument of perigee: | 94.7530° |
| revolutions per day: | 12.42891413 |
| mean anomaly at epoch: | 265.5200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|