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 46383U 26145.14470240 +.00000000 +00000-0 +57300-3 0 00005
2 46383 53.0393 297.8738 0003034 189.9062 170.1897 15.74652668 01
| Epoch (UTC): | 25 May 2026 03:28:22 |
| Eccentricity: | 0.0003034 |
| inclination: | 53.0393° |
| perigee height: | 344 km |
| apogee height: | 348 km |
| right ascension of ascending node: | 297.8738° |
| argument of perigee: | 189.9062° |
| revolutions per day: | 15.74652668 |
| mean anomaly at epoch: | 170.1897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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