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 64438U 26145.22743455 +.00000000 +00000-0 +76223-3 0 00001
2 64438 53.1595 92.8684 0000956 112.7200 247.3903 15.33570905 01
| Epoch (UTC): | 25 May 2026 05:27:30 |
| Eccentricity: | 0.0000956 |
| inclination: | 53.1595° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 92.8684° |
| argument of perigee: | 112.7200° |
| revolutions per day: | 15.33570905 |
| mean anomaly at epoch: | 247.3903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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