View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63983U 26145.61455044 +.00000000 +00000-0 +71268-3 0 00006
2 63983 97.3641 222.5975 0008703 26.1549 334.0133 15.37374510 01
| Epoch (UTC): | 25 May 2026 14:44:57 |
| Eccentricity: | 0.0008703 |
| inclination: | 97.3641° |
| perigee height: | 448 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 222.5975° |
| argument of perigee: | 26.1549° |
| revolutions per day: | 15.37374510 |
| mean anomaly at epoch: | 334.0133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|