View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 19120U 88039B 23155.77969705 .00000151 00000-0 94748-4 0 9990
2 19120 71.0159 41.3804 0019765 87.3492 272.9895 14.19318006815480
| Epoch (UTC): | 04 June 2023 18:42:45 |
| Eccentricity: | 0.0019765 |
| inclination: | 71.0159° |
| perigee height: | 813 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 41.3804° |
| argument of perigee: | 87.3492° |
| revolutions per day: | 14.19318006 |
| mean anomaly at epoch: | 272.9895° |
| orbit number at epoch: | 81548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|