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 64584U 26145.62375764 +.00000000 +00000-0 +26152-3 0 00007
2 64584 97.7396 262.5026 0001710 136.9597 223.1761 15.00913180 02
| Epoch (UTC): | 25 May 2026 14:58:12 |
| Eccentricity: | 0.0001710 |
| inclination: | 97.7396° |
| perigee height: | 563 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 262.5026° |
| argument of perigee: | 136.9597° |
| revolutions per day: | 15.00913180 |
| mean anomaly at epoch: | 223.1761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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