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 26101.47319111 +.00000000 +00000-0 +13610-4 0 00001
2 44909 82.5261 24.0333 0216548 300.5676 57.4216 12.79747941 06
| Epoch (UTC): | 11 April 2026 11:21:23 |
| Eccentricity: | 0.0216548 |
| inclination: | 82.5261° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 24.0333° |
| argument of perigee: | 300.5676° |
| revolutions per day: | 12.79747941 |
| mean anomaly at epoch: | 57.4216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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