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 63438U 26145.38966101 +.00000000 +00000-0 +95803-3 0 00007
2 63438 53.1598 143.6737 0000932 71.1725 288.9382 15.42178559 02
| Epoch (UTC): | 25 May 2026 09:21:06 |
| Eccentricity: | 0.0000932 |
| inclination: | 53.1598° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.6737° |
| argument of perigee: | 71.1725° |
| revolutions per day: | 15.42178559 |
| mean anomaly at epoch: | 288.9382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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