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 53560U 26145.20404973 +.00000000 +00000-0 +26899-5 0 00008
2 53560 53.2135 70.8168 0001322 83.9794 276.1349 15.08837449 09
| Epoch (UTC): | 25 May 2026 04:53:49 |
| Eccentricity: | 0.0001322 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 70.8168° |
| argument of perigee: | 83.9794° |
| revolutions per day: | 15.08837449 |
| mean anomaly at epoch: | 276.1349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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