View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 11326U 79030A 23334.18241149 .00000107 00000-0 95197-4 0 9990
2 11326 82.9499 14.7852 0029402 174.9384 245.2761 13.75492318474764
| Epoch (UTC): | 30 November 2023 04:22:40 |
| Eccentricity: | 0.0029402 |
| inclination: | 82.9499° |
| perigee height: | 958 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 14.7852° |
| argument of perigee: | 174.9384° |
| revolutions per day: | 13.75492318 |
| mean anomaly at epoch: | 245.2761° |
| orbit number at epoch: | 47476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|