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 40967U 15058D 25134.25256858 .00002357 00000-0 21543-3 0 9996
2 40967 64.7760 75.8654 0164655 203.9612 155.3777 14.87869751 54159
Epoch (UTC): | 14 May 2025 06:03:41 |
Eccentricity: | 0.0164655 |
inclination: | 64.7760° |
perigee height: | 489 km |
apogee height: | 719 km |
right ascension of ascending node: | 75.8654° |
argument of perigee: | 203.9612° |
revolutions per day: | 14.87869751 |
mean anomaly at epoch: | 155.3777° |
orbit number at epoch: | 5415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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