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 63766U 26145.52153831 +.00000000 +00000-0 +74639-3 0 00009
2 63766 43.0002 331.7079 0001333 269.0826 90.9873 15.27603611 00
| Epoch (UTC): | 25 May 2026 12:31:00 |
| Eccentricity: | 0.0001333 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.7079° |
| argument of perigee: | 269.0826° |
| revolutions per day: | 15.27603611 |
| mean anomaly at epoch: | 90.9873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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