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 64084U 26145.32629218 +.00000000 +00000-0 +27994-3 0 00000
2 64084 43.0007 128.5143 0000348 288.2196 71.8618 15.27586648 06
| Epoch (UTC): | 25 May 2026 07:49:51 |
| Eccentricity: | 0.0000348 |
| inclination: | 43.0007° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 128.5143° |
| argument of perigee: | 288.2196° |
| revolutions per day: | 15.27586648 |
| mean anomaly at epoch: | 71.8618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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