View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63979U 26145.55820244 +.00000000 +00000-0 +60449-3 0 00001
2 63979 42.9989 98.5179 0000424 331.0431 29.0397 15.27591428 05
| Epoch (UTC): | 25 May 2026 13:23:48 |
| Eccentricity: | 0.0000424 |
| inclination: | 42.9989° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 98.5179° |
| argument of perigee: | 331.0431° |
| revolutions per day: | 15.27591428 |
| mean anomaly at epoch: | 29.0397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|