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 66543U 26145.47198542 +.00000000 +00000-0 +66847-3 0 00009
2 66543 43.0023 204.5342 0001571 271.7677 88.2995 15.27593238 05
| Epoch (UTC): | 25 May 2026 11:19:39 |
| Eccentricity: | 0.0001571 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.5342° |
| argument of perigee: | 271.7677° |
| revolutions per day: | 15.27593238 |
| mean anomaly at epoch: | 88.2995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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