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 66620U 26145.37629229 +.00000000 +00000-0 +41489-3 0 00000
2 66620 53.1588 144.0214 0000986 93.9765 266.1348 15.30204194 09
| Epoch (UTC): | 25 May 2026 09:01:51 |
| Eccentricity: | 0.0000986 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.0214° |
| argument of perigee: | 93.9765° |
| revolutions per day: | 15.30204194 |
| mean anomaly at epoch: | 266.1348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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