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 31128U 07012M 25143.80750033 .00000853 00000-0 17019-3 0 9993
2 31128 98.3885 101.0736 0085986 213.0416 146.5396 14.62388444961418
Epoch (UTC): | 23 May 2025 19:22:48 |
Eccentricity: | 0.0085986 |
inclination: | 98.3885° |
perigee height: | 625 km |
apogee height: | 746 km |
right ascension of ascending node: | 101.0736° |
argument of perigee: | 213.0416° |
revolutions per day: | 14.62388444 |
mean anomaly at epoch: | 146.5396° |
orbit number at epoch: | 96141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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