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 23343U 94074B 23150.12675472 .00000413 00000-0 64960-4 0 9991
2 23343 97.8408 199.6255 0005338 277.2480 101.8028 14.77447885537559
Epoch (UTC): | 30 May 2023 03:02:31 |
Eccentricity: | 0.0005338 |
inclination: | 97.8408° |
perigee height: | 633 km |
apogee height: | 641 km |
right ascension of ascending node: | 199.6255° |
argument of perigee: | 277.2480° |
revolutions per day: | 14.77447885 |
mean anomaly at epoch: | 101.8028° |
orbit number at epoch: | 53755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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