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 64282U 26145.62327793 +.00000000 +00000-0 +41954-3 0 00008
2 64282 53.1559 119.4385 0001114 99.7153 260.3974 15.30202781 04
| Epoch (UTC): | 25 May 2026 14:57:31 |
| Eccentricity: | 0.0001114 |
| inclination: | 53.1559° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.4385° |
| argument of perigee: | 99.7153° |
| revolutions per day: | 15.30202781 |
| mean anomaly at epoch: | 260.3974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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