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 66064U 26145.00739197 +.00000000 +00000-0 +50863-3 0 00004
2 66064 53.1587 250.9575 0001151 89.9814 270.1318 15.30197900 00
| Epoch (UTC): | 25 May 2026 00:10:38 |
| Eccentricity: | 0.0001151 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 250.9575° |
| argument of perigee: | 89.9814° |
| revolutions per day: | 15.30197900 |
| mean anomaly at epoch: | 270.1318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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