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 64454U 26145.25004528 +.00000000 +00000-0 +72322-3 0 00009
2 64454 53.1594 95.1336 0001017 72.8070 287.3043 15.31695890 06
| Epoch (UTC): | 25 May 2026 06:00:03 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 95.1336° |
| argument of perigee: | 72.8070° |
| revolutions per day: | 15.31695890 |
| mean anomaly at epoch: | 287.3043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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