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 64714U 26145.62601405 +.00000000 +00000-0 +15165-3 0 00008
2 64714 70.0004 120.5263 0003981 265.8282 94.2422 14.98336722 06
| Epoch (UTC): | 25 May 2026 15:01:27 |
| Eccentricity: | 0.0003981 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 120.5263° |
| argument of perigee: | 265.8282° |
| revolutions per day: | 14.98336722 |
| mean anomaly at epoch: | 94.2422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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