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 64018U 26145.33335647 +.00000000 +00000-0 +20437-2 0 00002
2 64018 43.0022 285.1465 0001797 260.0028 203.6311 15.27556080 00
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001797 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 285.1465° |
| argument of perigee: | 260.0028° |
| revolutions per day: | 15.27556080 |
| mean anomaly at epoch: | 203.6311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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