View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00016U 58002A 25196.36627754 -.00000040 00000-0 -44926-4 0 9990
2 00016 34.2575 199.1392 2022899 138.1997 239.2161 10.49573276653528
Epoch (UTC): | 15 July 2025 08:47:26 |
Eccentricity: | 0.2022899 |
inclination: | 34.2575° |
perigee height: | 651 km |
apogee height: | 4216 km |
right ascension of ascending node: | 199.1392° |
argument of perigee: | 138.1997° |
revolutions per day: | 10.49573276 |
mean anomaly at epoch: | 239.2161° |
orbit number at epoch: | 65352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|