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 12443U 81041B 23151.70661190 .00000244 00000-0 94796-4 0 9999
2 12443 74.0521 147.6259 0003212 61.7247 298.4229 14.35037797199601
| Epoch (UTC): | 31 May 2023 16:57:31 |
| Eccentricity: | 0.0003212 |
| inclination: | 74.0521° |
| perigee height: | 772 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 147.6259° |
| argument of perigee: | 61.7247° |
| revolutions per day: | 14.35037797 |
| mean anomaly at epoch: | 298.4229° |
| orbit number at epoch: | 19960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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