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 25138.19223812 .00001414 00000-0 18845-3 0 9999
2 38756 98.2448 43.7056 0009604 245.4176 114.6035 14.81291121683837
Epoch (UTC): | 18 May 2025 04:36:49 |
Eccentricity: | 0.0009604 |
inclination: | 98.2448° |
perigee height: | 618 km |
apogee height: | 632 km |
right ascension of ascending node: | 43.7056° |
argument of perigee: | 245.4176° |
revolutions per day: | 14.81291121 |
mean anomaly at epoch: | 114.6035° |
orbit number at epoch: | 68383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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