View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39484U 13076B 23084.16003623 .00000009 00000-0 -93927-5 0 9998
2 39484 82.4927 185.0921 0022580 146.4712 213.7802 12.42881015419560
| Epoch (UTC): | 25 March 2023 03:50:27 |
| Eccentricity: | 0.0022580 |
| inclination: | 82.4927° |
| perigee height: | 1476 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 185.0921° |
| argument of perigee: | 146.4712° |
| revolutions per day: | 12.42881015 |
| mean anomaly at epoch: | 213.7802° |
| orbit number at epoch: | 41956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|