View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 09023U 76069B 23156.12209344 .00000294 00000-0 10148-3 0 9996
2 09023 74.0444 34.5438 0016955 18.8356 341.3422 14.40023606458106
| Epoch (UTC): | 05 June 2023 02:55:48 |
| Eccentricity: | 0.0016955 |
| inclination: | 74.0444° |
| perigee height: | 746 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 34.5438° |
| argument of perigee: | 18.8356° |
| revolutions per day: | 14.40023606 |
| mean anomaly at epoch: | 341.3422° |
| orbit number at epoch: | 45810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|