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 46486U 26145.58951287 +.00000000 +00000-0 +54379-3 0 00005
2 46486 82.5004 1.5629 0023468 84.3523 276.0232 12.42872477 06
| Epoch (UTC): | 25 May 2026 14:08:53 |
| Eccentricity: | 0.0023468 |
| inclination: | 82.5004° |
| perigee height: | 1476 km |
| apogee height: | 1513 km |
| right ascension of ascending node: | 1.5629° |
| argument of perigee: | 84.3523° |
| revolutions per day: | 12.42872477 |
| mean anomaly at epoch: | 276.0232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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