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 62483U 26145.52120508 +.00000000 +00000-0 +00000-0 0 00007
2 62483 0.0307 108.9214 0000162 84.6687 281.4607 1.00271655 03
| Epoch (UTC): | 25 May 2026 12:30:32 |
| Eccentricity: | 0.0000162 |
| inclination: | 0.0307° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 108.9214° |
| argument of perigee: | 84.6687° |
| revolutions per day: | 1.00271655 |
| mean anomaly at epoch: | 281.4607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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