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 63994U 26145.66332450 +.00000000 +00000-0 +71089-3 0 00009
2 63994 42.9986 283.5798 0000782 267.7631 92.3131 15.27601144 02
| Epoch (UTC): | 25 May 2026 15:55:11 |
| Eccentricity: | 0.0000782 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 283.5798° |
| argument of perigee: | 267.7631° |
| revolutions per day: | 15.27601144 |
| mean anomaly at epoch: | 92.3131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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