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 61663U 26145.26411813 +.00000000 +00000-0 +16339-4 0 00005
2 61663 53.1618 94.3970 0001309 84.0388 276.0764 15.34390373 04
| Epoch (UTC): | 25 May 2026 06:20:19 |
| Eccentricity: | 0.0001309 |
| inclination: | 53.1618° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 94.3970° |
| argument of perigee: | 84.0388° |
| revolutions per day: | 15.34390373 |
| mean anomaly at epoch: | 276.0764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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