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 26135.09071936 +.00000000 +00000-0 +10505-3 0 00005
2 44909 82.5237 1.7014 0216716 221.5727 136.8721 12.79748184 06
| Epoch (UTC): | 15 May 2026 02:10:38 |
| Eccentricity: | 0.0216716 |
| inclination: | 82.5237° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 1.7014° |
| argument of perigee: | 221.5727° |
| revolutions per day: | 12.79748184 |
| mean anomaly at epoch: | 136.8721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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