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 56128U 26145.17934705 +.00000000 +00000-0 +15330-4 0 00005
2 56128 43.0035 75.4110 0000768 262.0043 98.0721 15.27576760 08
| Epoch (UTC): | 25 May 2026 04:18:15 |
| Eccentricity: | 0.0000768 |
| inclination: | 43.0035° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 75.4110° |
| argument of perigee: | 262.0043° |
| revolutions per day: | 15.27576760 |
| mean anomaly at epoch: | 98.0721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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