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 51785U 26145.01499946 +.00000000 +00000-0 -24758-4 0 00000
2 51785 53.2134 356.4543 0001410 98.6889 261.4263 15.08831305 08
| Epoch (UTC): | 25 May 2026 00:21:35 |
| Eccentricity: | 0.0001410 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 356.4543° |
| argument of perigee: | 98.6889° |
| revolutions per day: | 15.08831305 |
| mean anomaly at epoch: | 261.4263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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