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 25194.16663687 .00000633 00000-0 65378-4 0 9991
2 41634 74.9983 200.0266 0005913 154.8634 205.2843 14.91952007490561
Epoch (UTC): | 13 July 2025 03:59:57 |
Eccentricity: | 0.0005913 |
inclination: | 74.9983° |
perigee height: | 588 km |
apogee height: | 596 km |
right ascension of ascending node: | 200.0266° |
argument of perigee: | 154.8634° |
revolutions per day: | 14.91952007 |
mean anomaly at epoch: | 205.2843° |
orbit number at epoch: | 49056 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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