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 25544U 26102.52168344 +.00000000 +00000-0 +11066-3 0 00004
2 25544 51.6322 265.0758 0006461 304.0419 55.9955 15.48885432 08
| Epoch (UTC): | 12 April 2026 12:31:13 |
| Eccentricity: | 0.0006461 |
| inclination: | 51.6322° |
| perigee height: | 416 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 265.0758° |
| argument of perigee: | 304.0419° |
| revolutions per day: | 15.48885432 |
| mean anomaly at epoch: | 55.9955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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