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 64912U 26144.98814484 +.00000000 +00000-0 +10533-2 0 00002
2 64912 53.1590 351.3983 0001141 72.5503 287.5622 15.30205520 03
| Epoch (UTC): | 24 May 2026 23:42:55 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.3983° |
| argument of perigee: | 72.5503° |
| revolutions per day: | 15.30205520 |
| mean anomaly at epoch: | 287.5622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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