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 15032U 84056B 25198.61442585 .00000109 00000-0 46442-4 0 9998
2 15032 74.0692 76.2920 0017640 216.0737 143.9227 14.35946760150167
Epoch (UTC): | 17 July 2025 14:44:46 |
Eccentricity: | 0.0017640 |
inclination: | 74.0692° |
perigee height: | 759 km |
apogee height: | 784 km |
right ascension of ascending node: | 76.2920° |
argument of perigee: | 216.0737° |
revolutions per day: | 14.35946760 |
mean anomaly at epoch: | 143.9227° |
orbit number at epoch: | 15016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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