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 63984U 26145.61811904 +.00000000 +00000-0 +45595-3 0 00002
2 63984 97.3671 218.9016 0032203 81.9820 278.5067 15.19900639 08
| Epoch (UTC): | 25 May 2026 14:50:05 |
| Eccentricity: | 0.0032203 |
| inclination: | 97.3671° |
| perigee height: | 484 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 218.9016° |
| argument of perigee: | 81.9820° |
| revolutions per day: | 15.19900639 |
| mean anomaly at epoch: | 278.5067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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