View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29507U 06046C 23155.80757470 .00002928 00000-0 21183-3 0 9992
2 29507 97.6874 189.0998 0045407 121.7023 238.8642 15.03985834907832
| Epoch (UTC): | 04 June 2023 19:22:54 |
| Eccentricity: | 0.0045407 |
| inclination: | 97.6874° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 189.0998° |
| argument of perigee: | 121.7023° |
| revolutions per day: | 15.03985834 |
| mean anomaly at epoch: | 238.8642° |
| orbit number at epoch: | 90783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|