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 26110.85472940 +.00000000 +00000-0 +41059-4 0 00001
2 44909 82.5263 17.8020 0216386 278.5196 79.1438 12.79747938 05
| Epoch (UTC): | 20 April 2026 20:30:48 |
| Eccentricity: | 0.0216386 |
| inclination: | 82.5263° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 17.8020° |
| argument of perigee: | 278.5196° |
| revolutions per day: | 12.79747938 |
| mean anomaly at epoch: | 79.1438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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