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 64313U 26145.29900440 +.00000000 +00000-0 +26820-3 0 00007
2 64313 70.0016 1.3088 0002448 270.2855 89.8024 14.98337339 01
| Epoch (UTC): | 25 May 2026 07:10:33 |
| Eccentricity: | 0.0002448 |
| inclination: | 70.0016° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3088° |
| argument of perigee: | 270.2855° |
| revolutions per day: | 14.98337339 |
| mean anomaly at epoch: | 89.8024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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