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 66496U 26145.36933373 +.00000000 +00000-0 +72291-3 0 00003
2 66496 43.0015 277.8576 0001516 268.8558 91.2120 15.27601532 00
| Epoch (UTC): | 25 May 2026 08:51:50 |
| Eccentricity: | 0.0001516 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.8576° |
| argument of perigee: | 268.8558° |
| revolutions per day: | 15.27601532 |
| mean anomaly at epoch: | 91.2120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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