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 44884U 26145.58201294 +.00000000 +00000-0 +36886-3 0 00004
2 44884 97.7830 235.4409 0016794 104.8328 255.4758 15.00411918 00
| Epoch (UTC): | 25 May 2026 13:58:05 |
| Eccentricity: | 0.0016794 |
| inclination: | 97.7830° |
| perigee height: | 554 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 235.4409° |
| argument of perigee: | 104.8328° |
| revolutions per day: | 15.00411918 |
| mean anomaly at epoch: | 255.4758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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