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 66483U 26145.21963520 +.00000000 +00000-0 +79585-3 0 00003
2 66483 43.0009 223.7070 0001806 276.6748 83.3898 15.27596390 07
| Epoch (UTC): | 25 May 2026 05:16:16 |
| Eccentricity: | 0.0001806 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 223.7070° |
| argument of perigee: | 276.6748° |
| revolutions per day: | 15.27596390 |
| mean anomaly at epoch: | 83.3898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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