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 66396U 26145.20775792 +.00000000 +00000-0 +54157-3 0 00005
2 66396 53.1583 220.5498 0001097 86.1044 274.0084 15.34411512 09
| Epoch (UTC): | 25 May 2026 04:59:10 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 220.5498° |
| argument of perigee: | 86.1044° |
| revolutions per day: | 15.34411512 |
| mean anomaly at epoch: | 274.0084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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