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 25347.89541822 .00011998 00000-0 22109-3 0 9995
2 25544 51.6304 136.7564 0003257 246.2023 113.8624 15.49578000543038
| Epoch (UTC): | 13 December 2025 21:29:24 |
| Eccentricity: | 0.0003257 |
| inclination: | 51.6304° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 136.7564° |
| argument of perigee: | 246.2023° |
| revolutions per day: | 15.49578000 |
| mean anomaly at epoch: | 113.8624° |
| orbit number at epoch: | 54303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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