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 41557U 16033B 23086.22885688 .00063038 00000-0 11339-2 0 9990
2 41557 97.3828 191.5055 0007329 93.2062 351.3544 15.49600664380894
| Epoch (UTC): | 27 March 2023 05:29:33 |
| Eccentricity: | 0.0007329 |
| inclination: | 97.3828° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 191.5055° |
| argument of perigee: | 93.2062° |
| revolutions per day: | 15.49600664 |
| mean anomaly at epoch: | 351.3544° |
| orbit number at epoch: | 38089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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