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 64287U 26145.62449176 +.00000000 +00000-0 +47396-4 0 00000
2 64287 86.5006 21.1397 0001766 98.6208 261.5126 13.24408238 08
| Epoch (UTC): | 25 May 2026 14:59:16 |
| Eccentricity: | 0.0001766 |
| inclination: | 86.5006° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.1397° |
| argument of perigee: | 98.6208° |
| revolutions per day: | 13.24408238 |
| mean anomaly at epoch: | 261.5126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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