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 66531U 26145.49497050 +.00000000 +00000-0 +73805-3 0 00006
2 66531 43.0022 203.8530 0002176 282.8880 77.1729 15.27590133 06
| Epoch (UTC): | 25 May 2026 11:52:45 |
| Eccentricity: | 0.0002176 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 203.8530° |
| argument of perigee: | 282.8880° |
| revolutions per day: | 15.27590133 |
| mean anomaly at epoch: | 77.1729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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