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 26101.16047447 +.00000000 +00000-0 +23984-4 0 00002
2 44909 82.5261 24.2410 0216562 301.3011 56.7045 12.79747933 05
| Epoch (UTC): | 11 April 2026 03:51:04 |
| Eccentricity: | 0.0216562 |
| inclination: | 82.5261° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 24.2410° |
| argument of perigee: | 301.3011° |
| revolutions per day: | 12.79747933 |
| mean anomaly at epoch: | 56.7045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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