View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63956U 26145.19366909 +.00000000 +00000-0 +66954-3 0 00006
2 63956 43.0007 104.4259 0001178 265.7361 94.3356 15.27583715 01
| Epoch (UTC): | 25 May 2026 04:38:53 |
| Eccentricity: | 0.0001178 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.4259° |
| argument of perigee: | 265.7361° |
| revolutions per day: | 15.27583715 |
| mean anomaly at epoch: | 94.3356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|