View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33938U 93036ET 24357.90231336 .00004243 00000-0 12236-2 0 9994
2 33938 74.0460 148.7726 0017251 320.1408 194.9960 14.44883822832711
| Epoch (UTC): | 22 December 2024 21:39:19 |
| Eccentricity: | 0.0017251 |
| inclination: | 74.0460° |
| perigee height: | 730 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 148.7726° |
| argument of perigee: | 320.1408° |
| revolutions per day: | 14.44883822 |
| mean anomaly at epoch: | 194.9960° |
| orbit number at epoch: | 83271 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|