View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 19573U 88093A 24357.64299693 .00009256 00000-0 43617-3 0 9998
2 19573 82.5231 198.3499 0012835 290.5782 69.4075 15.19300644952081
| Epoch (UTC): | 22 December 2024 15:25:54 |
| Eccentricity: | 0.0012835 |
| inclination: | 82.5231° |
| perigee height: | 499 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 198.3499° |
| argument of perigee: | 290.5782° |
| revolutions per day: | 15.19300644 |
| mean anomaly at epoch: | 69.4075° |
| orbit number at epoch: | 95208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|