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 62467U 26145.28159921 +.00000000 +00000-0 +85304-3 0 00006
2 62467 43.0008 121.6243 0001825 247.3174 112.7500 15.70856104 08
| Epoch (UTC): | 25 May 2026 06:45:30 |
| Eccentricity: | 0.0001825 |
| inclination: | 43.0008° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 121.6243° |
| argument of perigee: | 247.3174° |
| revolutions per day: | 15.70856104 |
| mean anomaly at epoch: | 112.7500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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