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 64281U 26145.35355751 +.00000000 +00000-0 +21443-2 0 00002
2 64281 53.1569 120.6043 0001032 58.1653 301.9448 15.30301602 02
| Epoch (UTC): | 25 May 2026 08:29:07 |
| Eccentricity: | 0.0001032 |
| inclination: | 53.1569° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.6043° |
| argument of perigee: | 58.1653° |
| revolutions per day: | 15.30301602 |
| mean anomaly at epoch: | 301.9448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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