View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39421U 26144.87063637 +.00000000 +00000-0 +26578-3 0 00000
2 39421 97.7040 115.2171 0029823 166.9153 193.2853 15.04783611 08
| Epoch (UTC): | 24 May 2026 20:53:42 |
| Eccentricity: | 0.0029823 |
| inclination: | 97.7040° |
| perigee height: | 532 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 115.2171° |
| argument of perigee: | 166.9153° |
| revolutions per day: | 15.04783611 |
| mean anomaly at epoch: | 193.2853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|