View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00012U 59001B 22274.40800247 .00000256 00000-0 14400-3 0 9995
2 00012 32.9000 305.3999 1664991 152.0595 218.0392 11.44697896375768
| Epoch (UTC): | 01 October 2022 09:47:31 |
| Eccentricity: | 0.1664991 |
| inclination: | 32.9000° |
| perigee height: | 553 km |
| apogee height: | 3323 km |
| right ascension of ascending node: | 305.3999° |
| argument of perigee: | 152.0595° |
| revolutions per day: | 11.44697896 |
| mean anomaly at epoch: | 218.0392° |
| orbit number at epoch: | 37576 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|