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 62446U 26145.26202833 +.00000000 +00000-0 +71929-3 0 00000
2 62446 53.1630 339.5100 0001560 90.0517 270.0663 15.30203540 04
| Epoch (UTC): | 25 May 2026 06:17:19 |
| Eccentricity: | 0.0001560 |
| inclination: | 53.1630° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 339.5100° |
| argument of perigee: | 90.0517° |
| revolutions per day: | 15.30203540 |
| mean anomaly at epoch: | 270.0663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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