View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 19238U 70025PT 22176.57596534 .00000831 00000-0 92829-3 0 9994
2 19238 99.8021 299.1940 0043833 244.3519 129.1337 13.74057240740445
| Epoch (UTC): | 25 June 2022 13:49:23 |
| Eccentricity: | 0.0043833 |
| inclination: | 99.8021° |
| perigee height: | 953 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 299.1940° |
| argument of perigee: | 244.3519° |
| revolutions per day: | 13.74057240 |
| mean anomaly at epoch: | 129.1337° |
| orbit number at epoch: | 74044 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|