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 38764U 26145.45281618 +.00000000 +00000-0 +51084-3 0 00005
2 38764 64.6420 162.6820 0046587 184.1591 175.9168 15.46606158 05
| Epoch (UTC): | 25 May 2026 10:52:03 |
| Eccentricity: | 0.0046587 |
| inclination: | 64.6420° |
| perigee height: | 395 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 162.6820° |
| argument of perigee: | 184.1591° |
| revolutions per day: | 15.46606158 |
| mean anomaly at epoch: | 175.9168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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