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 66651U 26145.53649804 +.00000000 +00000-0 +27183-3 0 00008
2 66651 97.7471 75.0073 0013700 70.2820 289.9877 14.93074969 05
| Epoch (UTC): | 25 May 2026 12:52:33 |
| Eccentricity: | 0.0013700 |
| inclination: | 97.7471° |
| perigee height: | 579 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 75.0073° |
| argument of perigee: | 70.2820° |
| revolutions per day: | 14.93074969 |
| mean anomaly at epoch: | 289.9877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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