View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 12465U 81046B 24284.51762503 .00020532 00000-0 73966-3 0 9992
2 12465 81.2392 181.8593 0026138 3.7467 356.3958 15.28113506359386
| Epoch (UTC): | 10 October 2024 12:25:22 |
| Eccentricity: | 0.0026138 |
| inclination: | 81.2392° |
| perigee height: | 463 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 181.8593° |
| argument of perigee: | 3.7467° |
| revolutions per day: | 15.28113506 |
| mean anomaly at epoch: | 356.3958° |
| orbit number at epoch: | 35938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|