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 22175.52037248 .00003133 00000-0 27282-3 0 9991
2 32788 97.5339 160.5846 0013461 96.8566 263.4188 14.97542716769494
| Epoch (UTC): | 24 June 2022 12:29:20 |
| Eccentricity: | 0.0013461 |
| inclination: | 97.5339° |
| perigee height: | 565 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 160.5846° |
| argument of perigee: | 96.8566° |
| revolutions per day: | 14.97542716 |
| mean anomaly at epoch: | 263.4188° |
| orbit number at epoch: | 76949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|