View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29U 60002B 24251.21984285 .00004162 00000-0 61456-3 0 9990
2 29 48.3766 220.3880 0023253 359.1238 0.9631 14.76751946446391
| Epoch (UTC): | 07 September 2024 05:16:34 |
| Eccentricity: | 0.0023253 |
| inclination: | 48.3766° |
| perigee height: | 623 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 220.3880° |
| argument of perigee: | 359.1238° |
| revolutions per day: | 14.76751946 |
| mean anomaly at epoch: | 0.9631° |
| orbit number at epoch: | 44639 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|