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 63847U 26145.32378115 +.00000000 +00000-0 +45753-3 0 00006
2 63847 42.9999 5.0032 0001062 71.3630 288.7337 15.27590798 02
| Epoch (UTC): | 25 May 2026 07:46:14 |
| Eccentricity: | 0.0001062 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.0032° |
| argument of perigee: | 71.3630° |
| revolutions per day: | 15.27590798 |
| mean anomaly at epoch: | 288.7337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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