View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39026U 12072A 23035.56217565 .00038235 00000-0 73828-3 0 9994
2 39026 97.2815 30.2495 0025902 47.2800 313.0625 15.47334223564667
| Epoch (UTC): | 04 February 2023 13:29:31 |
| Eccentricity: | 0.0025902 |
| inclination: | 97.2815° |
| perigee height: | 407 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 30.2495° |
| argument of perigee: | 47.2800° |
| revolutions per day: | 15.47334223 |
| mean anomaly at epoch: | 313.0625° |
| orbit number at epoch: | 56466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|