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 32788U 08021F 25139.97047148 .08158600 26426-5 14044-2 0 9997
2 32788 97.5714 139.5734 0010482 221.9933 138.0559 16.32875487930171
| Epoch (UTC): | 19 May 2025 23:17:28 |
| Eccentricity: | 0.0010482 |
| inclination: | 97.5714° |
| perigee height: | 178 km |
| apogee height: | 192 km |
| right ascension of ascending node: | 139.5734° |
| argument of perigee: | 221.9933° |
| revolutions per day: | 16.32875487 |
| mean anomaly at epoch: | 138.0559° |
| orbit number at epoch: | 93017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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