View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 19046U 88032B 25117.94284853 .00008777 00000-0 45515-3 0 9992
2 19046 97.4849 99.1161 0026315 250.5019 109.3371 15.16093848 4215
| Epoch (UTC): | 27 April 2025 22:37:42 |
| Eccentricity: | 0.0026315 |
| inclination: | 97.4849° |
| perigee height: | 499 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 99.1161° |
| argument of perigee: | 250.5019° |
| revolutions per day: | 15.16093848 |
| mean anomaly at epoch: | 109.3371° |
| orbit number at epoch: | 421 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|