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 62468U 26145.32394722 +.00000000 +00000-0 +19459-2 0 00009
2 62468 42.9992 121.0696 0001556 264.7219 95.3471 15.70917499 07
| Epoch (UTC): | 25 May 2026 07:46:29 |
| Eccentricity: | 0.0001556 |
| inclination: | 42.9992° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 121.0696° |
| argument of perigee: | 264.7219° |
| revolutions per day: | 15.70917499 |
| mean anomaly at epoch: | 95.3471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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