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 64473U 26145.35572307 +.00000000 +00000-0 +72929-3 0 00009
2 64473 53.1572 120.8874 0001222 98.3705 261.7434 15.30180262 03
| Epoch (UTC): | 25 May 2026 08:32:14 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.1572° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.8874° |
| argument of perigee: | 98.3705° |
| revolutions per day: | 15.30180262 |
| mean anomaly at epoch: | 261.7434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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