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 63863U 26145.61358352 +.00000000 +00000-0 +44016-3 0 00008
2 63863 42.9998 3.7134 0001021 274.1176 85.9559 15.27597348 01
| Epoch (UTC): | 25 May 2026 14:43:33 |
| Eccentricity: | 0.0001021 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.7134° |
| argument of perigee: | 274.1176° |
| revolutions per day: | 15.27597348 |
| mean anomaly at epoch: | 85.9559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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