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 25082.89117357 .00014132 00000-0 12054-2 0 9998
2 40967 64.7756 234.6800 0172246 219.9359 138.8979 14.87117550 46516
Epoch (UTC): | 23 March 2025 21:23:17 |
Eccentricity: | 0.0172246 |
inclination: | 64.7756° |
perigee height: | 486 km |
apogee height: | 727 km |
right ascension of ascending node: | 234.6800° |
argument of perigee: | 219.9359° |
revolutions per day: | 14.87117550 |
mean anomaly at epoch: | 138.8979° |
orbit number at epoch: | 4651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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