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 25349.89461712 .00006813 00000-0 12896-3 0 9998
2 25544 51.6305 126.8563 0003169 254.4589 105.6050 15.49611341543340
| Epoch (UTC): | 15 December 2025 21:28:14 |
| Eccentricity: | 0.0003169 |
| inclination: | 51.6305° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 126.8563° |
| argument of perigee: | 254.4589° |
| revolutions per day: | 15.49611341 |
| mean anomaly at epoch: | 105.6050° |
| orbit number at epoch: | 54334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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