View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33498U 09002G 24279.78110850 .00018354 00000-0 20282-2 0 9999
2 33498 98.1133 196.2876 0011542 53.9166 306.3117 14.87414634846108
| Epoch (UTC): | 05 October 2024 18:44:47 |
| Eccentricity: | 0.0011542 |
| inclination: | 98.1133° |
| perigee height: | 598 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 196.2876° |
| argument of perigee: | 53.9166° |
| revolutions per day: | 14.87414634 |
| mean anomaly at epoch: | 306.3117° |
| orbit number at epoch: | 84610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|