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 64590U 26145.28615513 +.00000000 +00000-0 +13618-3 0 00008
2 64590 97.7695 259.9831 0006528 58.0312 302.1542 14.93978458 01
| Epoch (UTC): | 25 May 2026 06:52:03 |
| Eccentricity: | 0.0006528 |
| inclination: | 97.7695° |
| perigee height: | 581 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 259.9831° |
| argument of perigee: | 58.0312° |
| revolutions per day: | 14.93978458 |
| mean anomaly at epoch: | 302.1542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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