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 62463U 26145.29221729 +.00000000 +00000-0 +16281-2 0 00006
2 62463 43.0008 121.7115 0002143 269.1399 90.9223 15.70889875 08
| Epoch (UTC): | 25 May 2026 07:00:47 |
| Eccentricity: | 0.0002143 |
| inclination: | 43.0008° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 121.7115° |
| argument of perigee: | 269.1399° |
| revolutions per day: | 15.70889875 |
| mean anomaly at epoch: | 90.9223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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