View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 34159U 97051EN 24358.02877214 .00002381 00000-0 79182-3 0 9991
2 34159 86.3535 199.2284 0029547 13.7923 346.4075 14.37091919828619
| Epoch (UTC): | 23 December 2024 00:41:25 |
| Eccentricity: | 0.0029547 |
| inclination: | 86.3535° |
| perigee height: | 747 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 199.2284° |
| argument of perigee: | 13.7923° |
| revolutions per day: | 14.37091919 |
| mean anomaly at epoch: | 346.4075° |
| orbit number at epoch: | 82861 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|