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 06324U 72104B 25192.59545943 .00000156 00000-0 52332-4 0 9993
2 06324 74.0769 42.3378 0008270 148.4499 211.7156 14.45055771760525
Epoch (UTC): | 11 July 2025 14:17:27 |
Eccentricity: | 0.0008270 |
inclination: | 74.0769° |
perigee height: | 736 km |
apogee height: | 748 km |
right ascension of ascending node: | 42.3378° |
argument of perigee: | 148.4499° |
revolutions per day: | 14.45055771 |
mean anomaly at epoch: | 211.7156° |
orbit number at epoch: | 76052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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