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 38756U 12047B 25131.91009676 .00001213 00000-0 16268-3 0 9996
2 38756 98.2455 37.2448 0009525 268.6608 91.3513 14.81273775682888
Epoch (UTC): | 11 May 2025 21:50:32 |
Eccentricity: | 0.0009525 |
inclination: | 98.2455° |
perigee height: | 618 km |
apogee height: | 632 km |
right ascension of ascending node: | 37.2448° |
argument of perigee: | 268.6608° |
revolutions per day: | 14.81273775 |
mean anomaly at epoch: | 91.3513° |
orbit number at epoch: | 68288 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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