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 65966U 26145.32953572 +.00000000 +00000-0 +52330-3 0 00005
2 65966 51.9039 1.8048 0000749 106.5364 253.5680 14.79945909 03
| Epoch (UTC): | 25 May 2026 07:54:31 |
| Eccentricity: | 0.0000749 |
| inclination: | 51.9039° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 1.8048° |
| argument of perigee: | 106.5364° |
| revolutions per day: | 14.79945909 |
| mean anomaly at epoch: | 253.5680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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