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 14552U 83122B 25196.94500302 .00000315 00000-0 33532-4 0 9998
2 14552 82.5224 192.1170 0017693 138.7618 221.4939 14.85547399225681
Epoch (UTC): | 15 July 2025 22:40:48 |
Eccentricity: | 0.0017693 |
inclination: | 82.5224° |
perigee height: | 599 km |
apogee height: | 624 km |
right ascension of ascending node: | 192.1170° |
argument of perigee: | 138.7618° |
revolutions per day: | 14.85547399 |
mean anomaly at epoch: | 221.4939° |
orbit number at epoch: | 22568 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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