View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 03338U 68066B 23336.73971375 .00000154 00000-0 15138-3 0 9993
2 03338 80.6631 75.9477 1131257 39.4497 328.3633 12.23157631464900
| Epoch (UTC): | 02 December 2023 17:45:11 |
| Eccentricity: | 0.1131257 |
| inclination: | 80.6631° |
| perigee height: | 678 km |
| apogee height: | 2479 km |
| right ascension of ascending node: | 75.9477° |
| argument of perigee: | 39.4497° |
| revolutions per day: | 12.23157631 |
| mean anomaly at epoch: | 328.3633° |
| orbit number at epoch: | 46490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|