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 63496U 26145.26458095 +.00000000 +00000-0 +80525-3 0 00001
2 63496 53.1594 144.2567 0000729 85.2130 274.8954 15.30202748 04
| Epoch (UTC): | 25 May 2026 06:20:59 |
| Eccentricity: | 0.0000729 |
| inclination: | 53.1594° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.2567° |
| argument of perigee: | 85.2130° |
| revolutions per day: | 15.30202748 |
| mean anomaly at epoch: | 274.8954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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