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 64349U 26145.39728051 +.00000000 +00000-0 +15817-3 0 00007
2 64349 70.0006 200.9795 0003748 266.4505 93.6226 14.98335042 00
| Epoch (UTC): | 25 May 2026 09:32:05 |
| Eccentricity: | 0.0003748 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.9795° |
| argument of perigee: | 266.4505° |
| revolutions per day: | 14.98335042 |
| mean anomaly at epoch: | 93.6226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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