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 23148.11590018 .00047414 00000-0 65077-3 0 9996
2 41557 97.3869 255.2447 0007883 203.9968 156.0921 15.57166690390505
| Epoch (UTC): | 28 May 2023 02:46:53 |
| Eccentricity: | 0.0007883 |
| inclination: | 97.3869° |
| perigee height: | 390 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 255.2447° |
| argument of perigee: | 203.9968° |
| revolutions per day: | 15.57166690 |
| mean anomaly at epoch: | 156.0921° |
| orbit number at epoch: | 39050 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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