View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33591U 09005A 24338.38327302 .00000519 00000-0 30118-3 0 9994
2 33591 99.0259 35.8041 0014000 171.5315 188.6095 14.13218639815522
| Epoch (UTC): | 03 December 2024 09:11:54 |
| Eccentricity: | 0.0014000 |
| inclination: | 99.0259° |
| perigee height: | 838 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 35.8041° |
| argument of perigee: | 171.5315° |
| revolutions per day: | 14.13218639 |
| mean anomaly at epoch: | 188.6095° |
| orbit number at epoch: | 81552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|