View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63958U 26145.31675073 +.00000000 +00000-0 +40896-3 0 00004
2 63958 43.0004 103.6266 0000632 240.9023 119.1766 15.27557361 02
| Epoch (UTC): | 25 May 2026 07:36:07 |
| Eccentricity: | 0.0000632 |
| inclination: | 43.0004° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.6266° |
| argument of perigee: | 240.9023° |
| revolutions per day: | 15.27557361 |
| mean anomaly at epoch: | 119.1766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|