View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39132U 13015C 25118.25910235 .00039192 00000-0 94620-3 0 9990
2 39132 64.8643 92.4522 0025344 288.0267 71.8109 15.40650672662103
| Epoch (UTC): | 28 April 2025 06:13:06 |
| Eccentricity: | 0.0025344 |
| inclination: | 64.8643° |
| perigee height: | 427 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 92.4522° |
| argument of perigee: | 288.0267° |
| revolutions per day: | 15.40650672 |
| mean anomaly at epoch: | 71.8109° |
| orbit number at epoch: | 66210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|