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 63457U 26145.39799697 +.00000000 +00000-0 +77643-3 0 00005
2 63457 53.1585 143.7123 0001104 88.3777 271.7355 15.42173626 08
| Epoch (UTC): | 25 May 2026 09:33:06 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1585° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.7123° |
| argument of perigee: | 88.3777° |
| revolutions per day: | 15.42173626 |
| mean anomaly at epoch: | 271.7355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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