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 63441U 26145.38904244 +.00000000 +00000-0 +88305-3 0 00000
2 63441 53.1593 143.6619 0000959 88.3143 271.7973 15.42167845 05
| Epoch (UTC): | 25 May 2026 09:20:13 |
| Eccentricity: | 0.0000959 |
| inclination: | 53.1593° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.6619° |
| argument of perigee: | 88.3143° |
| revolutions per day: | 15.42167845 |
| mean anomaly at epoch: | 271.7973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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