View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28647U 05016B 22142.66601193 .00004113 00000-0 24466-3 0 9996
2 28647 56.9969 254.4011 0119612 337.3473 22.2311 15.07601951166087
| Epoch (UTC): | 22 May 2022 15:59:03 |
| Eccentricity: | 0.0119612 |
| inclination: | 56.9969° |
| perigee height: | 461 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 254.4011° |
| argument of perigee: | 337.3473° |
| revolutions per day: | 15.07601951 |
| mean anomaly at epoch: | 22.2311° |
| orbit number at epoch: | 16608 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|