View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63290U 26145.54728909 +.00000000 +00000-0 +52927-4 0 00004
2 63290 82.4966 92.7951 0016177 62.4362 297.8358 12.42892126 04
| Epoch (UTC): | 25 May 2026 13:08:05 |
| Eccentricity: | 0.0016177 |
| inclination: | 82.4966° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 92.7951° |
| argument of perigee: | 62.4362° |
| revolutions per day: | 12.42892126 |
| mean anomaly at epoch: | 297.8358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|