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 64453U 26145.24042703 +.00000000 +00000-0 +67846-3 0 00009
2 64453 53.1598 92.2382 0000963 94.3481 265.7632 15.34401995 00
| Epoch (UTC): | 25 May 2026 05:46:12 |
| Eccentricity: | 0.0000963 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.2382° |
| argument of perigee: | 94.3481° |
| revolutions per day: | 15.34401995 |
| mean anomaly at epoch: | 265.7632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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