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 is defined by the following mean orbital elements,
1 25544U 26018.88513457 +.00000000 +00000-0 +23754-3 0 00005
2 25544 51.6336 318.5838 0007801 33.5888 326.5594 15.49391154 09
| Epoch (UTC): | 18 January 2026 21:14:35 |
| Eccentricity: | 0.0007801 |
| inclination: | 51.6336° |
| perigee height: | 413 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 318.5838° |
| argument of perigee: | 33.5888° |
| revolutions per day: | 15.49391154 |
| mean anomaly at epoch: | 326.5594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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