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 41634U 16043A 25198.19002892 .00000733 00000-0 75228-4 0 9999
2 41634 74.9984 192.4285 0005753 144.2370 215.9205 14.91957958491166
Epoch (UTC): | 17 July 2025 04:33:38 |
Eccentricity: | 0.0005753 |
inclination: | 74.9984° |
perigee height: | 588 km |
apogee height: | 596 km |
right ascension of ascending node: | 192.4285° |
argument of perigee: | 144.2370° |
revolutions per day: | 14.91957958 |
mean anomaly at epoch: | 215.9205° |
orbit number at epoch: | 49116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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