View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32955U 08025C 23088.49010426 .00000024 00000-0 10241-3 0 9993
2 32955 82.5077 4.4836 0021770 354.4825 5.6016 12.43328392673896
| Epoch (UTC): | 29 March 2023 11:45:45 |
| Eccentricity: | 0.0021770 |
| inclination: | 82.5077° |
| perigee height: | 1475 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 4.4836° |
| argument of perigee: | 354.4825° |
| revolutions per day: | 12.43328392 |
| mean anomaly at epoch: | 5.6016° |
| orbit number at epoch: | 67389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|