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 25407U 98045B 25189.53180363 -.00000095 00000-0 -23873-4 0 9991
2 25407 71.0121 335.0134 0006356 22.1690 337.9707 14.16142486392536
Epoch (UTC): | 08 July 2025 12:45:47 |
Eccentricity: | 0.0006356 |
inclination: | 71.0121° |
perigee height: | 834 km |
apogee height: | 843 km |
right ascension of ascending node: | 335.0134° |
argument of perigee: | 22.1690° |
revolutions per day: | 14.16142486 |
mean anomaly at epoch: | 337.9707° |
orbit number at epoch: | 39253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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