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 03230U 68040B 25198.62243560 .00001667 00000-0 13221-3 0 9991
2 03230 74.0317 73.2221 0025859 313.3395 46.5637 15.01234258 54714
Epoch (UTC): | 17 July 2025 14:56:18 |
Eccentricity: | 0.0025859 |
inclination: | 74.0317° |
perigee height: | 545 km |
apogee height: | 581 km |
right ascension of ascending node: | 73.2221° |
argument of perigee: | 313.3395° |
revolutions per day: | 15.01234258 |
mean anomaly at epoch: | 46.5637° |
orbit number at epoch: | 5471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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