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 41605U 16040G 23083.04811180 .00015416 00000-0 58044-3 0 9997
2 41605 97.1740 119.5316 0009349 233.0789 126.9594 15.27151039374946
| Epoch (UTC): | 24 March 2023 01:09:16 |
| Eccentricity: | 0.0009349 |
| inclination: | 97.1740° |
| perigee height: | 478 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 119.5316° |
| argument of perigee: | 233.0789° |
| revolutions per day: | 15.27151039 |
| mean anomaly at epoch: | 126.9594° |
| orbit number at epoch: | 37494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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