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 59503U 26144.75149329 +.00000000 +00000-0 -48602-4 0 00007
2 59503 43.0016 270.5884 0001421 271.1310 88.9378 15.27558661 04
| Epoch (UTC): | 24 May 2026 18:02:09 |
| Eccentricity: | 0.0001421 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.5884° |
| argument of perigee: | 271.1310° |
| revolutions per day: | 15.27558661 |
| mean anomaly at epoch: | 88.9378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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