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 25346.15413386 .00014398 00000-0 26408-3 0 9999
2 25544 51.6307 145.3792 0003284 237.6977 122.3694 15.49529746542766
| Epoch (UTC): | 12 December 2025 03:41:57 |
| Eccentricity: | 0.0003284 |
| inclination: | 51.6307° |
| perigee height: | 416 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 145.3792° |
| argument of perigee: | 237.6977° |
| revolutions per day: | 15.49529746 |
| mean anomaly at epoch: | 122.3694° |
| orbit number at epoch: | 54276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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