View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20046U 26139.40051176 +.00000000 +00000-0 +62536-4 0 00006
2 20046 82.9387 34.1331 0040627 290.3642 69.3153 13.78632219 00
| Epoch (UTC): | 19 May 2026 09:36:44 |
| Eccentricity: | 0.0040627 |
| inclination: | 82.9387° |
| perigee height: | 939 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 34.1331° |
| argument of perigee: | 290.3642° |
| revolutions per day: | 13.78632219 |
| mean anomaly at epoch: | 69.3153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|