View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 32709U 08011B 25187.99802541 .00003409 00000-0 18120-1 0 9991
2 32709 49.1072 76.7258 6527576 156.4466 257.1599 3.08963580135549
Epoch (UTC): | 06 July 2025 23:57:09 |
Eccentricity: | 0.6527576 |
inclination: | 49.1072° |
perigee height: | 536 km |
apogee height: | 26532 km |
right ascension of ascending node: | 76.7258° |
argument of perigee: | 156.4466° |
revolutions per day: | 3.08963580 |
mean anomaly at epoch: | 257.1599° |
orbit number at epoch: | 13554 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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