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 64352U 26145.43067587 +.00000000 +00000-0 +23623-3 0 00000
2 64352 70.0004 201.0970 0004002 268.1613 91.9088 14.98336668 04
| Epoch (UTC): | 25 May 2026 10:20:10 |
| Eccentricity: | 0.0004002 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.0970° |
| argument of perigee: | 268.1613° |
| revolutions per day: | 14.98336668 |
| mean anomaly at epoch: | 91.9088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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