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 20323U 89089B 25198.25473164 .00000179 00000-0 53205-4 0 9997
2 20323 97.1004 77.8553 0070117 145.2695 215.3110 14.50413930861600
Epoch (UTC): | 17 July 2025 06:06:48 |
Eccentricity: | 0.0070117 |
inclination: | 97.1004° |
perigee height: | 674 km |
apogee height: | 774 km |
right ascension of ascending node: | 77.8553° |
argument of perigee: | 145.2695° |
revolutions per day: | 14.50413930 |
mean anomaly at epoch: | 215.3110° |
orbit number at epoch: | 86160 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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