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 62462U 26145.28690763 +.00000000 +00000-0 +16925-2 0 00007
2 62462 42.9998 121.6701 0002175 270.6568 89.4051 15.70925064 06
| Epoch (UTC): | 25 May 2026 06:53:08 |
| Eccentricity: | 0.0002175 |
| inclination: | 42.9998° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 121.6701° |
| argument of perigee: | 270.6568° |
| revolutions per day: | 15.70925064 |
| mean anomaly at epoch: | 89.4051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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