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 66448U 26145.49554627 +.00000000 +00000-0 +80173-3 0 00003
2 66448 42.9998 200.9344 0001812 273.8439 86.2205 15.27594508 00
| Epoch (UTC): | 25 May 2026 11:53:35 |
| Eccentricity: | 0.0001812 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.9344° |
| argument of perigee: | 273.8439° |
| revolutions per day: | 15.27594508 |
| mean anomaly at epoch: | 86.2205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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