View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32788U 08021F 23086.66378343 .00013557 00000-0 10383-2 0 9996
2 32788 97.5585 68.0367 0004127 265.7952 94.2801 15.01970586810868
| Epoch (UTC): | 27 March 2023 15:55:50 |
| Eccentricity: | 0.0004127 |
| inclination: | 97.5585° |
| perigee height: | 558 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 68.0367° |
| argument of perigee: | 265.7952° |
| revolutions per day: | 15.01970586 |
| mean anomaly at epoch: | 94.2801° |
| orbit number at epoch: | 81086 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|