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 63442U 26145.38873830 +.00000000 +00000-0 +91422-3 0 00001
2 63442 53.1590 143.6688 0001336 58.5980 301.5156 15.42173693 00
| Epoch (UTC): | 25 May 2026 09:19:46 |
| Eccentricity: | 0.0001336 |
| inclination: | 53.1590° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 143.6688° |
| argument of perigee: | 58.5980° |
| revolutions per day: | 15.42173693 |
| mean anomaly at epoch: | 301.5156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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