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 46507U 26145.43883522 +.00000000 +00000-0 +45542-3 0 00001
2 46507 97.8626 151.6820 0006061 82.6526 277.5410 15.44890605 05
| Epoch (UTC): | 25 May 2026 10:31:55 |
| Eccentricity: | 0.0006061 |
| inclination: | 97.8626° |
| perigee height: | 428 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 151.6820° |
| argument of perigee: | 82.6526° |
| revolutions per day: | 15.44890605 |
| mean anomaly at epoch: | 277.5410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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