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 26088.10460712 +.00000000 +00000-0 -14518-4 0 00008
2 44909 82.5244 32.9132 0217063 331.9292 27.0239 12.79747751 04
| Epoch (UTC): | 29 March 2026 02:30:38 |
| Eccentricity: | 0.0217063 |
| inclination: | 82.5244° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 32.9132° |
| argument of perigee: | 331.9292° |
| revolutions per day: | 12.79747751 |
| mean anomaly at epoch: | 27.0239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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