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 62472U 26145.30271176 +.00000000 +00000-0 +12793-2 0 00003
2 62472 43.0024 120.8980 0001382 296.6064 63.4662 15.70966955 01
| Epoch (UTC): | 25 May 2026 07:15:54 |
| Eccentricity: | 0.0001382 |
| inclination: | 43.0024° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 120.8980° |
| argument of perigee: | 296.6064° |
| revolutions per day: | 15.70966955 |
| mean anomaly at epoch: | 63.4662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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