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 23154.10742566 .00000327 00000-0 11183-3 0 9997
2 09023 74.0445 38.2648 0016867 23.1973 336.9940 14.40022394457812
| Epoch (UTC): | 03 June 2023 02:34:41 |
| Eccentricity: | 0.0016867 |
| inclination: | 74.0445° |
| perigee height: | 746 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 38.2648° |
| argument of perigee: | 23.1973° |
| revolutions per day: | 14.40022394 |
| mean anomaly at epoch: | 336.9940° |
| orbit number at epoch: | 45781 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|