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 63418U 26144.97276306 +.00000000 +00000-0 +71261-3 0 00002
2 63418 43.0013 36.4573 0001498 277.3926 82.6755 15.27573545 08
| Epoch (UTC): | 24 May 2026 23:20:46 |
| Eccentricity: | 0.0001498 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 36.4573° |
| argument of perigee: | 277.3926° |
| revolutions per day: | 15.27573545 |
| mean anomaly at epoch: | 82.6755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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