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 62023U 26145.33471992 +.00000000 +00000-0 +25165-3 0 00004
2 62023 53.1602 171.8187 0001196 83.3811 276.7325 15.30199770 00
| Epoch (UTC): | 25 May 2026 08:01:59 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.8187° |
| argument of perigee: | 83.3811° |
| revolutions per day: | 15.30199770 |
| mean anomaly at epoch: | 276.7325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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