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 66472U 26145.54528888 +.00000000 +00000-0 +65333-3 0 00007
2 66472 43.0016 221.8580 0001663 287.2301 72.8369 15.27592809 09
| Epoch (UTC): | 25 May 2026 13:05:12 |
| Eccentricity: | 0.0001663 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.8580° |
| argument of perigee: | 287.2301° |
| revolutions per day: | 15.27592809 |
| mean anomaly at epoch: | 72.8369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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