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 66503U 26145.42957764 +.00000000 +00000-0 +73115-3 0 00005
2 66503 43.0012 277.4462 0001234 232.0657 128.0083 15.27593889 08
| Epoch (UTC): | 25 May 2026 10:18:35 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.4462° |
| argument of perigee: | 232.0657° |
| revolutions per day: | 15.27593889 |
| mean anomaly at epoch: | 128.0083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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