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 64073U 26145.63028764 +.00000000 +00000-0 +21152-2 0 00000
2 64073 43.0010 354.9225 0001439 255.5266 104.5442 15.70933699 00
| Epoch (UTC): | 25 May 2026 15:07:36 |
| Eccentricity: | 0.0001439 |
| inclination: | 43.0010° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 354.9225° |
| argument of perigee: | 255.5266° |
| revolutions per day: | 15.70933699 |
| mean anomaly at epoch: | 104.5442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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