View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39206U 13036A 23081.39469286 .00000051 00000-0 00000+0 0 9999
2 39206 2.9683 31.4881 0050763 183.1267 290.0811 1.00270465 35446
| Epoch (UTC): | 22 March 2023 09:28:21 |
| Eccentricity: | 0.0050763 |
| inclination: | 2.9683° |
| perigee height: | 35572 km |
| apogee height: | 36000 km |
| right ascension of ascending node: | 31.4881° |
| argument of perigee: | 183.1267° |
| revolutions per day: | 1.00270465 |
| mean anomaly at epoch: | 290.0811° |
| orbit number at epoch: | 3544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|