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 56529U 26145.43094198 +.00000000 +00000-0 +36078-4 0 00004
2 56529 43.0015 128.0093 0001320 283.7734 76.2970 15.25908481 09
| Epoch (UTC): | 25 May 2026 10:20:33 |
| Eccentricity: | 0.0001320 |
| inclination: | 43.0015° |
| perigee height: | 487 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 128.0093° |
| argument of perigee: | 283.7734° |
| revolutions per day: | 15.25908481 |
| mean anomaly at epoch: | 76.2970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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