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 21098.04788391 0.00000000 00000-0 00000-0 0 02
2 38109 122.9958 351.5237 0002002 127.4035 232.5964 13.41426316 03
Epoch (UTC): | 08 April 2021 01:08:57 |
Eccentricity: | 0.0002002 |
inclination: | 122.9958° |
perigee height: | 1102 km |
apogee height: | 1105 km |
right ascension of ascending node: | 351.5237° |
argument of perigee: | 127.4035° |
revolutions per day: | 13.41426316 |
mean anomaly at epoch: | 232.5964° |
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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