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 23081.77851774 .00057411 00000-0 10566-2 0 9993
2 41557 97.3827 186.9513 0008047 102.8150 16.3197 15.48964007380203
| Epoch (UTC): | 22 March 2023 18:41:03 |
| Eccentricity: | 0.0008047 |
| inclination: | 97.3827° |
| perigee height: | 414 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 186.9513° |
| argument of perigee: | 102.8150° |
| revolutions per day: | 15.48964007 |
| mean anomaly at epoch: | 16.3197° |
| orbit number at epoch: | 38020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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