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 29092U 06015A 23150.05140200 .00000826 00000-0 10522-3 0 9996
2 29092 97.8392 177.5884 0001529 92.6359 267.5030 14.84132607924434
| Epoch (UTC): | 30 May 2023 01:14:01 |
| Eccentricity: | 0.0001529 |
| inclination: | 97.8392° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 177.5884° |
| argument of perigee: | 92.6359° |
| revolutions per day: | 14.84132607 |
| mean anomaly at epoch: | 267.5030° |
| orbit number at epoch: | 92443 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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