View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20465U 90010A 25322.24420648 .00004509 00000-0 27413-3 0 9999
2 20465 82.4636 157.1297 0010514 7.0933 353.0443 15.10190522925412
| Epoch (UTC): | 18 November 2025 05:51:39 |
| Eccentricity: | 0.0010514 |
| inclination: | 82.4636° |
| perigee height: | 528 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 157.1297° |
| argument of perigee: | 7.0933° |
| revolutions per day: | 15.10190522 |
| mean anomaly at epoch: | 353.0443° |
| orbit number at epoch: | 92541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|