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 63198U 26144.91385950 +.00000000 +00000-0 +58660-3 0 00005
2 63198 43.0002 14.4965 0001496 274.1492 85.9189 15.27604602 09
| Epoch (UTC): | 24 May 2026 21:55:57 |
| Eccentricity: | 0.0001496 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 14.4965° |
| argument of perigee: | 274.1492° |
| revolutions per day: | 15.27604602 |
| mean anomaly at epoch: | 85.9189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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