View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00058U 60013A 23160.89760501 .00000124 00000-0 62292-4 0 9993
2 00058 28.3284 337.6646 0164827 72.4460 289.4021 13.46352630 85268
| Epoch (UTC): | 09 June 2023 21:32:33 |
| Eccentricity: | 0.0164827 |
| inclination: | 28.3284° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 337.6646° |
| argument of perigee: | 72.4460° |
| revolutions per day: | 13.46352630 |
| mean anomaly at epoch: | 289.4021° |
| orbit number at epoch: | 8526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|