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 04382U 70034A 23149.50598119 .00001216 00000-0 18860-3 0 9994
2 04382 68.4236 167.8052 1045601 261.3756 86.7671 13.09616490499459
Epoch (UTC): | 29 May 2023 12:08:36 |
Eccentricity: | 0.1045601 |
inclination: | 68.4236° |
perigee height: | 430 km |
apogee height: | 2019 km |
right ascension of ascending node: | 167.8052° |
argument of perigee: | 261.3756° |
revolutions per day: | 13.09616490 |
mean anomaly at epoch: | 86.7671° |
orbit number at epoch: | 49945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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