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 62443U 26145.54018139 +.00000000 +00000-0 +87972-3 0 00007
2 62443 53.1597 338.4097 0001057 94.0994 266.0128 15.30239576 09
| Epoch (UTC): | 25 May 2026 12:57:51 |
| Eccentricity: | 0.0001057 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.4097° |
| argument of perigee: | 94.0994° |
| revolutions per day: | 15.30239576 |
| mean anomaly at epoch: | 266.0128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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