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 66974U 26144.80872785 +.00000000 +00000-0 +58468-3 0 00001
2 66974 43.0003 313.1544 0001598 271.6536 88.4133 15.27593313 04
| Epoch (UTC): | 24 May 2026 19:24:34 |
| Eccentricity: | 0.0001598 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.1544° |
| argument of perigee: | 271.6536° |
| revolutions per day: | 15.27593313 |
| mean anomaly at epoch: | 88.4133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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