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 66473U 26145.52999132 +.00000000 +00000-0 -82693-4 0 00000
2 66473 43.0012 222.6038 0003712 265.9243 94.1184 15.27589320 04
| Epoch (UTC): | 25 May 2026 12:43:11 |
| Eccentricity: | 0.0003712 |
| inclination: | 43.0012° |
| perigee height: | 480 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 222.6038° |
| argument of perigee: | 265.9243° |
| revolutions per day: | 15.27589320 |
| mean anomaly at epoch: | 94.1184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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