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 63483U 26145.57809296 +.00000000 +00000-0 +54636-3 0 00008
2 63483 43.0016 185.7161 0001523 253.5895 106.4789 15.27598434 00
| Epoch (UTC): | 25 May 2026 13:52:27 |
| Eccentricity: | 0.0001523 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.7161° |
| argument of perigee: | 253.5895° |
| revolutions per day: | 15.27598434 |
| mean anomaly at epoch: | 106.4789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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