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 66741U 26145.14290622 +.00000000 +00000-0 +35941-3 0 00006
2 66741 97.4250 219.2167 0007138 78.1924 282.0111 15.20167598 00
| Epoch (UTC): | 25 May 2026 03:25:47 |
| Eccentricity: | 0.0007138 |
| inclination: | 97.4250° |
| perigee height: | 500 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 219.2167° |
| argument of perigee: | 78.1924° |
| revolutions per day: | 15.20167598 |
| mean anomaly at epoch: | 282.0111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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