View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 23439U 94085A 24256.91670419 -.00000016 00000-0 75874-3 0 9995
2 23439 64.8136 261.8951 0147686 127.1893 234.2616 11.27578547223486
| Epoch (UTC): | 12 September 2024 22:00:03 |
| Eccentricity: | 0.0147686 |
| inclination: | 64.8136° |
| perigee height: | 1898 km |
| apogee height: | 2146 km |
| right ascension of ascending node: | 261.8951° |
| argument of perigee: | 127.1893° |
| revolutions per day: | 11.27578547 |
| mean anomaly at epoch: | 234.2616° |
| orbit number at epoch: | 22348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|