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 25544U 98067A 25343.89682520 .00014877 00000-0 27325-3 0 9996
2 25544 51.6313 156.5563 0003347 226.2924 133.7787 15.49459040542419
| Epoch (UTC): | 09 December 2025 21:31:25 |
| Eccentricity: | 0.0003347 |
| inclination: | 51.6313° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 156.5563° |
| argument of perigee: | 226.2924° |
| revolutions per day: | 15.49459040 |
| mean anomaly at epoch: | 133.7787° |
| orbit number at epoch: | 54241 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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