View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 35685U 09041E 23336.87523878 .00002564 00000-0 28640-3 0 9996
2 35685 98.1101 56.6814 0055065 327.1280 32.6514 14.86836368776311
| Epoch (UTC): | 02 December 2023 21:00:20 |
| Eccentricity: | 0.0055065 |
| inclination: | 98.1101° |
| perigee height: | 569 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 56.6814° |
| argument of perigee: | 327.1280° |
| revolutions per day: | 14.86836368 |
| mean anomaly at epoch: | 32.6514° |
| orbit number at epoch: | 77631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|