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 66589U 26145.24190706 +.00000000 +00000-0 +60542-3 0 00004
2 66589 42.9985 343.8495 0001756 275.4040 84.6612 15.27596167 06
| Epoch (UTC): | 25 May 2026 05:48:20 |
| Eccentricity: | 0.0001756 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.8495° |
| argument of perigee: | 275.4040° |
| revolutions per day: | 15.27596167 |
| mean anomaly at epoch: | 84.6612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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