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 53656U 26145.61579811 +.00000000 +00000-0 -11758-3 0 00000
2 53656 97.4484 25.5769 0002370 76.7112 283.4379 15.05658176 03
| Epoch (UTC): | 25 May 2026 14:46:44 |
| Eccentricity: | 0.0002370 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.5769° |
| argument of perigee: | 76.7112° |
| revolutions per day: | 15.05658176 |
| mean anomaly at epoch: | 283.4379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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