View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32787U 08021E 25143.95035351 .00042017 00000-0 93302-3 0 9998
2 32787 97.6431 133.3349 0008524 88.1802 272.0422 15.43549597929686
Epoch (UTC): | 23 May 2025 22:48:30 |
Eccentricity: | 0.0008524 |
inclination: | 97.6431° |
perigee height: | 430 km |
apogee height: | 441 km |
right ascension of ascending node: | 133.3349° |
argument of perigee: | 88.1802° |
revolutions per day: | 15.43549597 |
mean anomaly at epoch: | 272.0422° |
orbit number at epoch: | 92968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|