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 38109U 12014A 25136.04770598 0.00000000 00000-0 00000-0 0 09
2 38109 123.0012 323.4146 0008427 19.0857 340.9143 13.41427266 06
Epoch (UTC): | 16 May 2025 01:08:41 |
Eccentricity: | 0.0008427 |
inclination: | 123.0012° |
perigee height: | 1097 km |
apogee height: | 1110 km |
right ascension of ascending node: | 323.4146° |
argument of perigee: | 19.0857° |
revolutions per day: | 13.41427266 |
mean anomaly at epoch: | 340.9143° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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