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 66459U 26145.57484356 +.00000000 +00000-0 +91592-3 0 00002
2 66459 43.0017 222.0833 0001580 277.6712 82.3960 15.27585593 01
| Epoch (UTC): | 25 May 2026 13:47:46 |
| Eccentricity: | 0.0001580 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.0833° |
| argument of perigee: | 277.6712° |
| revolutions per day: | 15.27585593 |
| mean anomaly at epoch: | 82.3960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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