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 14820U 84027B 23152.89241830 .00000563 00000-0 64167-4 0 9996
2 14820 82.5412 112.5371 0020230 80.9881 279.3623 14.84205936 97460
| Epoch (UTC): | 01 June 2023 21:25:04 |
| Eccentricity: | 0.0020230 |
| inclination: | 82.5412° |
| perigee height: | 602 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 112.5371° |
| argument of perigee: | 80.9881° |
| revolutions per day: | 14.84205936 |
| mean anomaly at epoch: | 279.3623° |
| orbit number at epoch: | 9746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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