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 82U 61004B 25200.28859698 .00000269 00000-0 26894-3 0 9994
2 82 38.8530 156.1450 1166974 54.6920 315.7374 12.27672657 35891
| Epoch (UTC): | 19 July 2025 06:55:34 |
| Eccentricity: | 0.1166974 |
| inclination: | 38.8530° |
| perigee height: | 633 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 156.1450° |
| argument of perigee: | 54.6920° |
| revolutions per day: | 12.27672657 |
| mean anomaly at epoch: | 315.7374° |
| orbit number at epoch: | 3589 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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