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 64492U 26145.31905194 +.00000000 +00000-0 +97675-3 0 00005
2 64492 53.1598 118.5217 0001123 81.3142 278.7988 15.35414244 01
| Epoch (UTC): | 25 May 2026 07:39:26 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.1598° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 118.5217° |
| argument of perigee: | 81.3142° |
| revolutions per day: | 15.35414244 |
| mean anomaly at epoch: | 278.7988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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