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 23155.88937017 .00057727 00000-0 76541-3 0 9998
2 41557 97.3886 263.3022 0007856 180.0432 180.0824 15.58050067391718
| Epoch (UTC): | 04 June 2023 21:20:41 |
| Eccentricity: | 0.0007856 |
| inclination: | 97.3886° |
| perigee height: | 388 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 263.3022° |
| argument of perigee: | 180.0432° |
| revolutions per day: | 15.58050067 |
| mean anomaly at epoch: | 180.0824° |
| orbit number at epoch: | 39171 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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