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 62465U 26145.33987113 +.00000000 +00000-0 +14064-2 0 00006
2 62465 43.0022 121.2004 0002621 259.1125 100.9447 15.70899113 01
| Epoch (UTC): | 25 May 2026 08:09:24 |
| Eccentricity: | 0.0002621 |
| inclination: | 43.0022° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 121.2004° |
| argument of perigee: | 259.1125° |
| revolutions per day: | 15.70899113 |
| mean anomaly at epoch: | 100.9447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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