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 26066.44917759 +.00000000 +00000-0 -65601-5 0 00009
2 44909 82.5199 47.3033 0218020 22.5478 338.5026 12.79747421 04
| Epoch (UTC): | 07 March 2026 10:46:48 |
| Eccentricity: | 0.0218020 |
| inclination: | 82.5199° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 47.3033° |
| argument of perigee: | 22.5478° |
| revolutions per day: | 12.79747421 |
| mean anomaly at epoch: | 338.5026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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