View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00046U 60007B 25140.53599219 .00000982 00000-0 19866-3 0 9990
2 00046 66.6884 217.9234 0203017 229.7442 128.5763 14.53956204399902
| Epoch (UTC): | 20 May 2025 12:51:49 |
| Eccentricity: | 0.0203017 |
| inclination: | 66.6884° |
| perigee height: | 569 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 217.9234° |
| argument of perigee: | 229.7442° |
| revolutions per day: | 14.53956204 |
| mean anomaly at epoch: | 128.5763° |
| orbit number at epoch: | 39990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|