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 23159.55383588 .00000611 00000-0 83324-4 0 9999
2 32376 97.8883 343.1553 0001407 90.9702 269.1672 14.82145510838372
| Epoch (UTC): | 08 June 2023 13:17:31 |
| Eccentricity: | 0.0001407 |
| inclination: | 97.8883° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 343.1553° |
| argument of perigee: | 90.9702° |
| revolutions per day: | 14.82145510 |
| mean anomaly at epoch: | 269.1672° |
| orbit number at epoch: | 83837 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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