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 46496U 26145.59658461 +.00000000 +00000-0 +38766-3 0 00007
2 46496 97.7483 111.1091 0009434 56.6540 303.5602 15.30934297 01
| Epoch (UTC): | 25 May 2026 14:19:04 |
| Eccentricity: | 0.0009434 |
| inclination: | 97.7483° |
| perigee height: | 467 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 111.1091° |
| argument of perigee: | 56.6540° |
| revolutions per day: | 15.30934297 |
| mean anomaly at epoch: | 303.5602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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