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 64354U 26145.40562980 +.00000000 +00000-0 +17500-3 0 00003
2 64354 70.0008 201.0103 0003804 265.0951 94.9774 14.98334737 08
| Epoch (UTC): | 25 May 2026 09:44:06 |
| Eccentricity: | 0.0003804 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.0103° |
| argument of perigee: | 265.0951° |
| revolutions per day: | 14.98334737 |
| mean anomaly at epoch: | 94.9774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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