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 66151U 26145.19716737 +.00000000 +00000-0 +80109-3 0 00002
2 66151 53.1599 66.6220 0001180 88.2293 271.8844 15.34402794 00
| Epoch (UTC): | 25 May 2026 04:43:55 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 66.6220° |
| argument of perigee: | 88.2293° |
| revolutions per day: | 15.34402794 |
| mean anomaly at epoch: | 271.8844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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