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 63452U 26145.36268208 +.00000000 +00000-0 +11229-2 0 00003
2 63452 53.1584 143.4864 0001017 88.8821 271.2302 15.42169564 02
| Epoch (UTC): | 25 May 2026 08:42:15 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.1584° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.4864° |
| argument of perigee: | 88.8821° |
| revolutions per day: | 15.42169564 |
| mean anomaly at epoch: | 271.2302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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