View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63651U 26145.42516588 +.00000000 +00000-0 +39885-3 0 00007
2 63651 42.9968 291.7504 0000199 88.1900 271.8974 15.27577388 05
| Epoch (UTC): | 25 May 2026 10:12:14 |
| Eccentricity: | 0.0000199 |
| inclination: | 42.9968° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 291.7504° |
| argument of perigee: | 88.1900° |
| revolutions per day: | 15.27577388 |
| mean anomaly at epoch: | 271.8974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|