View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 38799U 99025EUP 23333.16853709 .00006316 00000-0 17381-2 0 9992
2 38799 98.4700 44.8807 0194599 75.6989 286.5719 14.36653490688100
| Epoch (UTC): | 29 November 2023 04:02:41 |
| Eccentricity: | 0.0194599 |
| inclination: | 98.4700° |
| perigee height: | 630 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 44.8807° |
| argument of perigee: | 75.6989° |
| revolutions per day: | 14.36653490 |
| mean anomaly at epoch: | 286.5719° |
| orbit number at epoch: | 68810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|