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 64585U 26145.55907097 +.00000000 +00000-0 +14536-3 0 00003
2 64585 97.7734 260.3951 0003000 87.3360 272.8202 14.91881245 09
| Epoch (UTC): | 25 May 2026 13:25:03 |
| Eccentricity: | 0.0003000 |
| inclination: | 97.7734° |
| perigee height: | 590 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 260.3951° |
| argument of perigee: | 87.3360° |
| revolutions per day: | 14.91881245 |
| mean anomaly at epoch: | 272.8202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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