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 44323U 26145.63204858 +.00000000 +00000-0 +21976-4 0 00002
2 44323 97.7594 153.4892 0001513 90.4280 269.7112 14.92588730 09
| Epoch (UTC): | 25 May 2026 15:10:08 |
| Eccentricity: | 0.0001513 |
| inclination: | 97.7594° |
| perigee height: | 589 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 153.4892° |
| argument of perigee: | 90.4280° |
| revolutions per day: | 14.92588730 |
| mean anomaly at epoch: | 269.7112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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