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 01328U 26053.74722659 +.00000000 +00000-0 +94639-4 0 00000
2 01328 41.1820 146.9444 0241413 70.7844 291.8864 13.38918681 05
| Epoch (UTC): | 22 February 2026 17:56:00 |
| Eccentricity: | 0.0241413 |
| inclination: | 41.1820° |
| perigee height: | 932 km |
| apogee height: | 1294 km |
| right ascension of ascending node: | 146.9444° |
| argument of perigee: | 70.7844° |
| revolutions per day: | 13.38918681 |
| mean anomaly at epoch: | 291.8864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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