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 65546U 26145.44124853 +.00000000 +00000-0 +75234-4 0 00003
2 65546 85.9923 54.2969 0001992 93.5725 266.5686 14.12445355 04
| Epoch (UTC): | 25 May 2026 10:35:23 |
| Eccentricity: | 0.0001992 |
| inclination: | 85.9923° |
| perigee height: | 850 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 54.2969° |
| argument of perigee: | 93.5725° |
| revolutions per day: | 14.12445355 |
| mean anomaly at epoch: | 266.5686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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