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 23608U 95033D 25196.58593270 .00014866 00000-0 48927-3 0 9999
2 23608 98.2920 5.0619 0011026 144.7086 215.4885 15.31572708630339
Epoch (UTC): | 15 July 2025 14:03:44 |
Eccentricity: | 0.0011026 |
inclination: | 98.2920° |
perigee height: | 463 km |
apogee height: | 478 km |
right ascension of ascending node: | 5.0619° |
argument of perigee: | 144.7086° |
revolutions per day: | 15.31572708 |
mean anomaly at epoch: | 215.4885° |
orbit number at epoch: | 63033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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