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 66383U 26145.46620345 +.00000000 +00000-0 +61628-3 0 00003
2 66383 53.1597 219.3229 0000782 24.3161 335.7878 15.34399917 02
| Epoch (UTC): | 25 May 2026 11:11:19 |
| Eccentricity: | 0.0000782 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.3229° |
| argument of perigee: | 24.3161° |
| revolutions per day: | 15.34399917 |
| mean anomaly at epoch: | 335.7878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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