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 64065U 26145.29645889 +.00000000 +00000-0 +14617-2 0 00004
2 64065 43.0007 356.7132 0001019 37.9607 322.1333 15.70878260 08
| Epoch (UTC): | 25 May 2026 07:06:54 |
| Eccentricity: | 0.0001019 |
| inclination: | 43.0007° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 356.7132° |
| argument of perigee: | 37.9607° |
| revolutions per day: | 15.70878260 |
| mean anomaly at epoch: | 322.1333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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