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 32376U 07059A 23150.84500827 .00000502 00000-0 69660-4 0 9995
2 32376 97.8884 334.5729 0001307 93.3034 266.8329 14.82161451837088
| Epoch (UTC): | 30 May 2023 20:16:48 |
| Eccentricity: | 0.0001307 |
| inclination: | 97.8884° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 334.5729° |
| argument of perigee: | 93.3034° |
| revolutions per day: | 14.82161451 |
| mean anomaly at epoch: | 266.8329° |
| orbit number at epoch: | 83708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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