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 25199.38078070 .00000101 00000-0 43638-4 0 9993
2 15032 74.0692 74.8880 0017610 214.5306 145.4704 14.35946952150270
Epoch (UTC): | 18 July 2025 09:08:19 |
Eccentricity: | 0.0017610 |
inclination: | 74.0692° |
perigee height: | 759 km |
apogee height: | 784 km |
right ascension of ascending node: | 74.8880° |
argument of perigee: | 214.5306° |
revolutions per day: | 14.35946952 |
mean anomaly at epoch: | 145.4704° |
orbit number at epoch: | 15027 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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