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 64623U 26145.43379323 +.00000000 +00000-0 +18306-3 0 00007
2 64623 97.4407 148.5749 0012968 210.3690 149.6794 15.18004328 01
| Epoch (UTC): | 25 May 2026 10:24:39 |
| Eccentricity: | 0.0012968 |
| inclination: | 97.4407° |
| perigee height: | 503 km |
| apogee height: | 521 km |
| right ascension of ascending node: | 148.5749° |
| argument of perigee: | 210.3690° |
| revolutions per day: | 15.18004328 |
| mean anomaly at epoch: | 149.6794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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