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 66148U 26145.07741690 +.00000000 +00000-0 +31203-3 0 00002
2 66148 53.1590 67.2944 0001403 105.1716 254.9442 15.34395483 06
| Epoch (UTC): | 25 May 2026 01:51:28 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 67.2944° |
| argument of perigee: | 105.1716° |
| revolutions per day: | 15.34395483 |
| mean anomaly at epoch: | 254.9442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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