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 64485U 26145.62226939 +.00000000 +00000-0 +82683-3 0 00007
2 64485 53.1562 119.6963 0001263 78.9718 281.1424 15.30198353 08
| Epoch (UTC): | 25 May 2026 14:56:04 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.1562° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.6963° |
| argument of perigee: | 78.9718° |
| revolutions per day: | 15.30198353 |
| mean anomaly at epoch: | 281.1424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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