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 64555U 26145.58420596 +.00000000 +00000-0 +14124-3 0 00000
2 64555 97.4658 260.8332 0002235 76.2736 283.8748 15.20247190 04
| Epoch (UTC): | 25 May 2026 14:01:15 |
| Eccentricity: | 0.0002235 |
| inclination: | 97.4658° |
| perigee height: | 504 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 260.8332° |
| argument of perigee: | 76.2736° |
| revolutions per day: | 15.20247190 |
| mean anomaly at epoch: | 283.8748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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