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 41604U 16040F 23083.06583845 .00014571 00000-0 53722-3 0 9991
2 41604 97.1740 121.8560 0009878 213.9588 146.1020 15.27853123375091
| Epoch (UTC): | 24 March 2023 01:34:48 |
| Eccentricity: | 0.0009878 |
| inclination: | 97.1740° |
| perigee height: | 475 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 121.8560° |
| argument of perigee: | 213.9588° |
| revolutions per day: | 15.27853123 |
| mean anomaly at epoch: | 146.1020° |
| orbit number at epoch: | 37509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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