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 64540U 26145.32371367 +.00000000 +00000-0 +59051-3 0 00005
2 64540 97.4590 262.6577 0001995 248.9779 111.1249 15.31773974 06
| Epoch (UTC): | 25 May 2026 07:46:08 |
| Eccentricity: | 0.0001995 |
| inclination: | 97.4590° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 262.6577° |
| argument of perigee: | 248.9779° |
| revolutions per day: | 15.31773974 |
| mean anomaly at epoch: | 111.1249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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