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 61578U 26145.58335647 +.00000000 +00000-0 -10607-2 0 00006
2 61578 53.1565 276.9919 0001166 101.8313 131.2203 15.69756985 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001166 |
| inclination: | 53.1565° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 276.9919° |
| argument of perigee: | 101.8313° |
| revolutions per day: | 15.69756985 |
| mean anomaly at epoch: | 131.2203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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