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 66430U 26145.45442235 +.00000000 +00000-0 +49726-3 0 00000
2 66430 42.9989 200.6342 0001283 281.3438 78.7269 15.27562930 01
| Epoch (UTC): | 25 May 2026 10:54:22 |
| Eccentricity: | 0.0001283 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.6342° |
| argument of perigee: | 281.3438° |
| revolutions per day: | 15.27562930 |
| mean anomaly at epoch: | 78.7269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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