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 66619U 26145.43106279 +.00000000 +00000-0 +48032-3 0 00001
2 66619 53.1575 143.6544 0001372 87.3084 272.8074 15.30185046 09
| Epoch (UTC): | 25 May 2026 10:20:43 |
| Eccentricity: | 0.0001372 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.6544° |
| argument of perigee: | 87.3084° |
| revolutions per day: | 15.30185046 |
| mean anomaly at epoch: | 272.8074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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