View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20U 59007A 25168.24052570 .00000696 00000-0 26494-3 0 9999
2 20 33.3511 139.8373 1643075 258.5654 82.6636 11.60705516442200
| Epoch (UTC): | 17 June 2025 05:46:21 |
| Eccentricity: | 0.1643075 |
| inclination: | 33.3511° |
| perigee height: | 508 km |
| apogee height: | 3215 km |
| right ascension of ascending node: | 139.8373° |
| argument of perigee: | 258.5654° |
| revolutions per day: | 11.60705516 |
| mean anomaly at epoch: | 82.6636° |
| orbit number at epoch: | 44220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|