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 44909U 26112.18378663 +.00000000 +00000-0 +56574-4 0 00004
2 44909 82.5262 16.9192 0216378 275.3943 82.2509 12.79747951 09
| Epoch (UTC): | 22 April 2026 04:24:39 |
| Eccentricity: | 0.0216378 |
| inclination: | 82.5262° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 16.9192° |
| argument of perigee: | 275.3943° |
| revolutions per day: | 12.79747951 |
| mean anomaly at epoch: | 82.2509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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