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 63455U 26145.37401001 +.00000000 +00000-0 +72645-3 0 00007
2 63455 53.1591 143.5585 0001109 77.0696 283.0434 15.42181943 08
| Epoch (UTC): | 25 May 2026 08:58:34 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1591° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.5585° |
| argument of perigee: | 77.0696° |
| revolutions per day: | 15.42181943 |
| mean anomaly at epoch: | 283.0434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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