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 64530U 26145.58188067 +.00000000 +00000-0 +47481-3 0 00009
2 64530 97.4592 261.5153 0003383 261.2588 98.8267 15.26289075 03
| Epoch (UTC): | 25 May 2026 13:57:54 |
| Eccentricity: | 0.0003383 |
| inclination: | 97.4592° |
| perigee height: | 485 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 261.5153° |
| argument of perigee: | 261.2588° |
| revolutions per day: | 15.26289075 |
| mean anomaly at epoch: | 98.8267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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