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 12472U 81049A 25193.45278802 -.00000265 00000-0 00000-0 0 9998
2 12472 9.9676 317.8893 0002002 284.9024 142.7509 1.00289722119445
Epoch (UTC): | 12 July 2025 10:52:00 |
Eccentricity: | 0.0002002 |
inclination: | 9.9676° |
perigee height: | 35773 km |
apogee height: | 35789 km |
right ascension of ascending node: | 317.8893° |
argument of perigee: | 284.9024° |
revolutions per day: | 1.00289722 |
mean anomaly at epoch: | 142.7509° |
orbit number at epoch: | 11944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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