View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00020U 59007A 23038.24657239 .00003916 00000-0 16120-2 0 9998
2 00020 33.3487 343.3601 1660120 347.0736 9.1822 11.56693152342277
| Epoch (UTC): | 07 February 2023 05:55:03 |
| Eccentricity: | 0.1660120 |
| inclination: | 33.3487° |
| perigee height: | 510 km |
| apogee height: | 3252 km |
| right ascension of ascending node: | 343.3601° |
| argument of perigee: | 347.0736° |
| revolutions per day: | 11.56693152 |
| mean anomaly at epoch: | 9.1822° |
| orbit number at epoch: | 34227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|