View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39008U 26144.97405737 +.00000000 +00000-0 +00000-0 0 00002
2 39008 0.0145 322.5103 0002266 105.0287 104.1918 1.00269717 04
| Epoch (UTC): | 24 May 2026 23:22:38 |
| Eccentricity: | 0.0002266 |
| inclination: | 0.0145° |
| perigee height: | 35778 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 322.5103° |
| argument of perigee: | 105.0287° |
| revolutions per day: | 1.00269717 |
| mean anomaly at epoch: | 104.1918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|