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 23079.30738490 .00056826 00000-0 10562-2 0 9993
2 41557 97.3819 184.4234 0007958 110.9436 278.7807 15.48685705379827
| Epoch (UTC): | 20 March 2023 07:22:38 |
| Eccentricity: | 0.0007958 |
| inclination: | 97.3819° |
| perigee height: | 415 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 184.4234° |
| argument of perigee: | 110.9436° |
| revolutions per day: | 15.48685705 |
| mean anomaly at epoch: | 278.7807° |
| orbit number at epoch: | 37982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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