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 23152.93782326 .00000577 00000-0 79073-4 0 9994
2 32376 97.8883 336.6354 0001327 93.8565 266.2800 14.82164500837390
| Epoch (UTC): | 01 June 2023 22:30:27 |
| Eccentricity: | 0.0001327 |
| inclination: | 97.8883° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 336.6354° |
| argument of perigee: | 93.8565° |
| revolutions per day: | 14.82164500 |
| mean anomaly at epoch: | 266.2800° |
| orbit number at epoch: | 83739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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