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 23152.12770177 .00000554 00000-0 76126-4 0 9997
2 32376 97.8883 335.8370 0001323 93.4699 266.6666 14.82163377837350
| Epoch (UTC): | 01 June 2023 03:03:53 |
| Eccentricity: | 0.0001323 |
| inclination: | 97.8883° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 335.8370° |
| argument of perigee: | 93.4699° |
| revolutions per day: | 14.82163377 |
| mean anomaly at epoch: | 266.6666° |
| orbit number at epoch: | 83735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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